MAINTENANCE MANUAL

and
INSTRUCTIONS FOR CONTINUED
AIRWORTHINESS
for
Raisbeck Systems
as installed on

TEXTRON’S BEECHCRAFT
KING AIR & SUPER KING AIR
MODEL AIRCRAFT

Models Raisbeck Systems

 B300/B300C  Quiet Turbofan Propellers
 300/300LW  Ram Air Recovery System
 200/B200/B200GT Series  Enhanced Performance Leading Edges
 100/A100/B100  Composite Exhaust Stack Fairings
 G90XT  Dual Aft Body Strakes
 F90  Fully-Enclosed MLG
 E90  Wing Lockers
 C90/C90A/C90GT/C90GTi  Swept Turbofan Propellers
 65-90/65-A90/B90

Document No. 85-120

Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

Log of Revisions
Rev Section Description Date Approved By
AK Various Added inspection, maintenance, and ICA 9/18/19 MJS
requirements for 200 Series Five-Blade Swept
Turbofan Propeller System.
05 Updated inspections to align with Beech.
See DCN AK for details.
AL Title Clarified make and model. 3/3/22 Tim Morgan
Introduction Updated referenced OEM maintenance
documents.
Introduction, Replaced all references to obsolete Hartzell
05, 12, 30, 61 Manuals 181, 182, & 183 with Manual No. 180.
05, 61 Typographical corrections. (ER 20-614)
05 Added Alternate Phase Inspection and Biennial
Inspection requirements, Sections 05-20-00-07,
-08, & -09. (ER 18-508, 21-663)
05 Removed Fully Enclosed MLG Doors RH
lubrication requirement from “Phase 3 or
Detailed 3 Inspections”, Section 05-20-00-03.
(ER 21-632)
12 Added figures that identify locker and latch
types, Sections 12-50-10-20 & 12-50-11-20.
(ER 20-606)
05, 12, 30 Added missing references to Hartzell Manual
No. 486, Sections 05-61-00-00, 05-61-00-21,
12-30-61-20, 30-61-00-05, & 30-61-00-20.
30 Corrected circuit breaker amperage notation,
Section 30-61-40-97, Figure 2. (ER 20-607)
12, 61 Corrected Hartzell Owner’s Manual No. for 200
Series composite propellers, Sections
12-61-42-20, 61-00-42-10, & 61-00-42-20.
(ER 21-630)
61 Added Five-Blade Swept, Section 60-00-40-05.
61 Removed references to nonexistent Figure 1
from Section 61-31-42-20.
61 Corrected Section number from 61-72-20-20 to
61-76-20-20.
61 Corrected propeller restricted range tolerance
from ±50 to +50/-0 RPM, Sections 61-76-20-20
& 61-76-30-20. (ER 20-621)
61 Corrected Power Symmetry and Low Pitch
Torque Check instructions, Section
61-76-42-20. (ER 21-665)
61 Updated Section 61-76-42-20 Figures 3 and 4
to correspond with installation clarifications.
AM 61-76-42-20 Corrected propeller restricted range caution
notes and added caution notes specific to
Collins Pro Line 21 or Pro Line Fusion
equipped aircraft.

Revision AM i
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

Introduction
The purpose of this manual is to give the necessary data for the normal maintenance of any Raisbeck
System installed on Beechcraft King Air or Super King Air. Chapter 51 gives data for acceptable
repairs and repair limits for selected Raisbeck Systems components. All data given in Chapter 51 are
approved by the Federal Aviation Administration (FAA), Northwest Mountain Region on December
22, 1992. Service Publication reissues or revisions are not automatically provided to the holder of
this manual.
Information in this document is given as supplemental to the applicable Original Equipment
Manufacturers (OEM) model and/or component specific documents listed below at the revision listed,
or later revision:
King Air Series and Super King Air Series Aircraft Manuals:
Maintenance Manuals (MM)
King Air 90 Series Maintenance Manual, P/N 90-590012-13, Revision D0, Dated December
1, 2019
King Air F90 Series Maintenance Manual, P/N 109-590010-19, Revision B7, Dated May 1,
2014
King Air 100 Series Maintenance Manual, P/N 100-590038-17, Revision A33, Dated February
1, 2017
Super King Air 200 Series Maintenance Manual, P/N 101-590010-19, Revision E1, Dated
November 1, 2019
Super King Air Model 300 and 300LW Maintenance Manual, P/N 101-590097-9, Revision
A38, Dated November 11, 2016
Super King Air B300/B300C Maintenance Manual, P/N 130-590031-11, Revision C3, Dated
October 15, 2020
Component Maintenance Manuals (CMM)
King Air Series Component Maintenance Manual, P/N 101-590097-13, Revision B9, Dated
April 1, 2018
Structural Repair Manuals (SRM)
Structural Inspection and Repair Manual, P/N 98-39006, Revision D2, Dated January 1, 2020

Nextant Aerospace for Model G90XT:

NOTE: G90XT aircraft are C90A aircraft modified per Nextant Aerospace STC
SA01902CH.
Nextant Airplane Flight Manual Supplement, NX0250-AFMS-0101, Revision C, October 22, 2015
Aircraft Maintenance Manual Supplement, NX0250-MMS0-0101, Revision A, December 19, 2015
Instructions for Continued Airworthiness, NX0250-ICA0-0101, Revision A, December 19, 2015
GE Turboprop Engines H80-100/H80-200 H75-100/H75-200 H85-100/H85-200 Maintenance
Manual, Document No. 0983402, Rev 13, Dated Feb. 15, 2017

Revision AM ii
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

Hartzell Propeller Inc. Turboprop Aluminum Propeller Systems:

Propeller Owner’s Manual and Logbook, Manual No. 149, 61-00-49, Revision 28, June 2021
Propeller Ice Protection System Manual, Manual No. 180, 30-61-80, Revision 36, June 2021

Hartzell Propeller Inc. Turboprop Composite Propeller Systems:

Propeller Owner’s Manual and Logbook, Manual No. 147, Revision 17, September 2020
Propeller Owner’s Manual and Logbook, Manual No. 486, Revision 4, June 2021
Composite Propeller Blade Field Maintenance and Minor Repair Manual, Manual No. 170,
Revision 17, July 2021
Propeller Ice Protection System Manual, Manual No. 180, 30-61-80, Revision 36, June 2021
Goodrich/UTC Aerospace Systems De-Icing and Specialty Systems:
Black Standard Pneumatic De-Icer Installation, Maintenance and Repair Manual, ATA 30-10-31,
Revision Original Issue, 15 Nov/96
Component Maintenance Manual, Brush Assemblies, Electrothermal De-Icing Systems, ATA 30-
60-01, Revised March 24, 2015
Installation and Maintenance Manual for Prop De-Icing Systems, ATA 30-60-02, Revised March
20, 2002
Removal and Installation Manual, Electrothermal Propeller De-Icers, ATA 30-60-07, July 14, 2007
SMR Technologies:
Pneumatic De-Icer Installation, Maintenance Manual, and Instructions for continued Airworthiness
SMR Report No. 97-33-047, February 20, 2019 (Rev. 16)

NOTE: Always use the most current revision of the manuals listed above.

Revision AM iii
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

Commercial Parts
Maintenance on Raisbeck Systems involving the replacement of Commercial Parts (as defined in
FAA Advisory Circular No. 21-45) should reference the latest revision of either the Illustrated Parts
Catalog, document 85-119, or the following Supplemental Type Certificate (STC) specific Commercial
Parts Lists (CPL) for accepted parts.
Commercial Parts Lists
Dual Aft Body Strakes:
200/A200/B200 Series, STC SA3591NM, reference CPL document 16BC-3591-090
300 Series, STC SA4733NM, reference CPL document 16BC-4733-090
B300 Series, STC SA5151NM, reference CPL document 16BC-5151-090
Exhaust Stack Fairings:
90 Series, 100 Series, F90, 200/A200/B200 Series, and 300/B300 Series, STC SA3683NM,
reference CPL document 17BC-3683-090
Enhanced Performance Leading Edge:
200/A200/B200 Series, STC SA3831NM, reference CPL document 16BC-3831-090
Nacelle Wing Locker System:
90 Series, STC SA2939NM, reference CPL document 16BC-2939-090
100 Series, STC SA3819NM, reference CPL document 17BC-3819-090
F90, STC SA4132NM, reference CPL document 17BC-4132-090
200/A200/B200 Series, STC SA3857NM, reference CPL document 16BC-3857-090
300 Series, STC SA4734NM, reference CPL document 16BC-4734-090
B300 Series, STC SA5152NM, reference CPL document 16BC-5152-090
Ram Air Recovery System:
200/A200/B200 Series, STC SA3366NM, reference CPL document 16BC-3366-090

NOTICE
Raisbeck Engineering specifically reserves the right to supersede, cancel, and/or declare inactive any
part number, kit, or publication that may be referenced in this manual without prior notice.

WARNING
Use only genuine Raisbeck or Beechcraft approved parts in connection with the maintenance and
repair of Raisbeck Systems.
Do not use the data in this Maintenance Manual for the installation of any Raisbeck System. Specific
FAA-Approved Installation Manuals for Raisbeck Systems are supplied with each kit purchased.

Revision AM iv
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

Correspondence
Raisbeck Engineering, Inc.
4411 South Ryan Way
Seattle, WA 98178
Telephone:
Domestic (206) 723-2000
International (800) 537-7277
Facsimile (206) 723-2884

Company website: www.raisbeck.com

Technical Support:
e-mail techsupport@raisbeck.com
AOG (206) 390-8690

Spare Parts:
e-mail spares@raisbeck.com
AOG (206) 390-8690

Organization
This Manual is arranged according to ATA Code by Chapter, Section, System, and Subject.
Example:
12-30-57-20
Chapter 12 Servicing
Section 30 Ice and Rain Protection
System 57 Wings (Enhanced Performance Leading Edges)
Subject 20 Standard Practices (Maintenance Procedures)

Revision AM v
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

Eligibility
KING AIR 90 SERIES AIRCRAFT
The Raisbeck Dual Aft Body Strake system is approved by the FAA under STC SA4010NM.
The Raisbeck Fully Enclosed Main Landing Gear Door system is approved by the FAA under STC
SA2623NM.
The Raisbeck Nacelle Wing Locker system is approved by the FAA under STC SA2939NM.
The Raisbeck Exhaust Stack Fairing system is approved by the FAA under STC SA3683NM.
The Raisbeck/Hartzell Quiet Turbofan Propeller system is approved by the FAA under STC
SA3593NM.
The Raisbeck/Hartzell Swept Turbofan Propeller system is approved by the FAA under STC
SA3593NM.

KING AIR F90 AIRCRAFT

The Raisbeck Dual Aft Body Strake system is approved by the FAA under STC SA4130NM.
The Raisbeck Fully Enclosed Main Landing Gear Door system is approved by the FAA under STC
SA4944NM.
The Raisbeck Nacelle Wing Locker system is approved by the FAA under STC SA4132NM.
The Raisbeck Exhaust Stack Fairing system is approved by the FAA under STC SA3683NM
The Raisbeck/Hartzell Quiet Turbofan Propeller system is approved by the FAA under STC
SA4131NM.

KING AIR 100 SERIES AIRCRAFT

The Raisbeck Dual Aft Body Strake system is approved by the FAA under STC SA3828NM.
The Raisbeck Fully Enclosed Main Landing Gear Door system is approved by the FAA under STC
SA4952NM.
The Raisbeck Nacelle Wing Locker system is approved by the FAA under STC SA3819NM.`
The Raisbeck Exhaust Stack Fairing system is approved by the FAA under STC SA3683NM
The Raisbeck/Hartzell Quiet Turbofan Propeller system is approved by the FAA under STC
SA5661NM.

Revision AM vi
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

SUPER KING AIR 200 SERIES AIRCRAFT

The Raisbeck Dual Aft Body Strake system is approved by the FAA under STC SA3591NM.
The Raisbeck Fully Enclosed Main Landing Gear Door system is approved by the FAA under STC
SA4175NM.
The Raisbeck Nacelle Wing Locker system is approved by the FAA under STC SA3857NM.
The Raisbeck Exhaust Stack Fairing system is approved by the FAA under STC SA3683NM
The Raisbeck/Hartzell Quiet Turbofan Propeller system is approved by the FAA under STC
SA2698NM-S.
The Raisbeck/Hartzell Swept Turbofan Propeller system is approved by the FAA under STC
SA2698NM-S.
The Raisbeck/Hartzell Five-Blade Swept Turbofan Propeller System is approved by the FAA under
STC SA2698NM-S.
The Raisbeck Enhanced Performance Leading Edge system is approved by the FAA under STC
SA3831NM.
The Raisbeck Ram Air Recovery System is approved by the FAA under STC SA3366NM.

SUPER KING AIR B200 SERIES AIRCRAFT

The Raisbeck Dual Aft Body Strake system is approved by the FAA under STC SA3591NM.
The Raisbeck Fully Enclosed Main Landing Gear Door system is approved by the FAA under STC
SA4175NM.
The Raisbeck Nacelle Wing Locker system is approved by the FAA under STC SA3857NM.
The Raisbeck Exhaust Stack Fairing system is approved by the FAA under STC SA3683NM
The Raisbeck/Hartzell Quiet Turbofan Propeller system is approved by the FAA under STC
SA2698NM-S.
The Raisbeck/Hartzell Swept Turbofan Propeller system is approved by the FAA under STC
SA2698NM-S.
The Raisbeck/Hartzell Five-Blade Swept Turbofan Propeller System is approved by the FAA under
STC SA2698NM-S.
The Raisbeck Enhanced Performance Leading Edge system is approved by the FAA under STC
SA3831NM.
The installation of the Raisbeck Enhanced Performance Leading Edge (SA3831NM), Dual Aft Body
Strakes (SA3591NM), Ram Air Recovery Systems (SA3366NM), High Flotation Gear Doors
(SA4175NM), and Hartzell/Beechcraft Turbofan Propeller System in accordance with Raisbeck
Engineering Master Drawing List 99-1500 requires the incorporation of Supplemental Type
Certificates SA4175NM (when equipped with high flotation gear), SA3366NM, SA3831NM, and
SA3591NM is approved by the FAA under STC SA00752SE.

Revision AM vii
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

SUPER KING AIR 300/300LW AIRCRAFT

The Raisbeck Dual Aft Body Strake system is approved by the FAA under STC SA4733NM.
The Raisbeck Fully Enclosed Main Landing Gear Door system is approved by the FAA under STC
SA4175NM.
The Raisbeck Nacelle Wing Locker system is approved by the FAA under STC SA4734NM.
The Raisbeck Exhaust Stack Fairing system is approved by the FAA under STC SA3683NM
The Raisbeck/Hartzell Four-Blade Swept Turbofan Propeller System is approved by the FAA under
STC SA02473SE.
The Raisbeck/Hartzell Five-Blade Swept Turbofan Propeller System is approved by the FAA under
STC SA02559SE.

SUPER KING AIR B300/B300C AIRCRAFT

The Raisbeck Dual Aft Body Strake system is approved by the FAA under STC SA5151NM.
The Raisbeck Fully Enclosed Main Landing Gear Door system is approved by the FAA under STC
SA4175NM.
The Raisbeck Nacelle Wing Locker system is approved by the FAA under STC SA5152NM.
The Raisbeck Exhaust Stack Fairing system is approved by the FAA under STC SA3683NM
The installation of the Raisbeck Dual Aft Body Strake system per (STC) SA5151NM and
Raisbeck/Hartzell Four-Blade Swept Turbofan Propeller system is approved by the FAA under STC
SA02473SE.
The installation of the Raisbeck Dual Aft Body Strake system per (STC) SA5151NM and
Raisbeck/Hartzell Five-blade Swept Turbofan Propeller system is approved by the FAA under STC
SA02559SE.

Revision AM viii
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

Table of Contents
00  Chapter Descriptions ............................................................................................................ 1 
04  Airworthiness Limitations .............................................................................................................. 1 
05  Time Limits/Maintenance Checks .................................................................................................. 1 
11  Placards .......................................................................................................................................... 1 
12  Servicing ......................................................................................................................................... 1 
20  Standard Practices Airframe .......................................................................................................... 1 
30  Ice and Rain Protection .................................................................................................................. 1 
32  Landing Gear .................................................................................................................................. 1 
50  Cargo and Accessory Compartments ............................................................................................. 1 
51  Standard Practices Structures ........................................................................................................ 2 
53  Fuselage ......................................................................................................................................... 2 
54  Nacelles/Pylons .............................................................................................................................. 2 
57  Wings ............................................................................................................................................. 2 
61  Propellers ....................................................................................................................................... 2 
04  Airworthiness Limitations .................................................................................................... 3 
04‐00‐00‐01  Mandatory Modification, Replacement, and Structural Inspection for Airframe Systems ............ 3 
04‐61‐00‐01  Mandatory Modification, Replacement, and Structural Inspection for Propellers ........................ 3 
04‐00‐00‐02  Mandatory Replacement Time, Inspection Intervals, and Procedures for Fuel Tanks ................... 3 
04‐00‐00‐03  Mandatory Replacement Time for EWIS Components ................................................................... 3 
04‐00‐00‐04  Limits of Validity of Engineering Data for Structural Maintenance ............................................... 3 
04‐00‐00‐05  Instructions for Continued Airworthiness ....................................................................................... 3 
05  Time Limit/Maintenance Checks .......................................................................................... 4 
05‐00‐00‐00  Description ..................................................................................................................................... 4 
05‐20‐00‐00  Scheduled Inspection...................................................................................................................... 4 
Daily Checks ........................................................................................................................................................... 5 
Phase Inspections .................................................................................................................................................. 6 
Fusion Inspections ................................................................................................................................................. 7 
HUIP Inspections .................................................................................................................................................... 8 
Alternate Phase Inspections .................................................................................................................................. 9 
Biennial Inspections ............................................................................................................................................... 9 
Daily Checklist ...................................................................................................................................................... 10 
05‐20‐00‐01  Scheduled Inspection Program Phase 1 or Detailed 1 Inspection ................................................ 13 
05‐20‐00‐01  Phase 1 or Detailed 1 Inspection Discrepancy Sheet .................................................................... 20 
05‐20‐00‐02  Scheduled Inspection Program Phase 2 or Detailed 2 Inspection ................................................ 21 
05‐20‐00‐02  Phase 2 or Detailed 2 Inspection Discrepancy Sheet .................................................................... 27 
05‐20‐00‐03  Scheduled Inspection Program Phase 3 or Detailed 3 Inspection ................................................ 28 
05‐20‐00‐03  Phase 3 or Detailed 3 Inspection Discrepancy Sheet .................................................................... 35 
05‐20‐00‐04  Scheduled Inspection Program Phase 4 or Detailed 4 Inspection ................................................ 36 
05‐20‐00‐04  Phase 4 or Detailed 4 Inspection Discrepancy Sheet .................................................................... 42 
05‐20‐00‐05  HUIP Routine Inspection .............................................................................................................. 43 
05‐20‐00‐05  HUIP Routine Inspection Discrepancy Sheet ................................................................................ 47 
05‐20‐00‐06  HUIP Inspection:  Detailed 1, 2, 3, & 4 ......................................................................................... 48 

Revision AM ix
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05‐20‐00‐06  HUIP Inspection:  Detailed 1, 2, 3, & 4 Discrepancy Sheet ........................................................... 54 
05‐20‐00‐07  Alternate Phase Inspection .......................................................................................................... 55 
05‐20‐00‐08  Biennial:  Interim Inspection ........................................................................................................ 55 
05‐20‐00‐08  Biennial:  Interim Inspection Discrepancy Sheet .......................................................................... 59 
05‐20‐00‐09  Biennial:  Complete Inspection ..................................................................................................... 60 
05‐20‐00‐09  Biennial:  Complete Inspection Discrepancy Sheet ....................................................................... 68 
05‐21‐00‐00  Special Inspection Maintenance Practices ................................................................................... 69 
05‐32‐00‐21  Fully Enclosed MLG Doors Special Inspections ............................................................................. 70 
05‐50‐00‐21  Wing Lockers Special Inspections ................................................................................................. 72 
05‐51‐00‐00  Time Limits/Maintenance Checks Airframe Systems ................................................................... 73 
05‐61‐00‐00  Time Limits/Maintenance Checks ‐ Propellers ............................................................................. 73 
05‐53‐00‐21  Dual Aft Body Strakes Special Inspections ................................................................................... 74 
05‐54‐00‐21  Exhaust Stack Fairings Special Inspections .................................................................................. 75 
05‐57‐00‐21  Enhanced Performance Leading Edges Special Inspections ......................................................... 76 
05‐61‐00‐21  Swept Turbofan Propellers, Five‐Blade Swept Turbofan Propellers, and Quiet Turbofan 
Propellers Special Inspections ...................................................................................................... 77 
05‐72‐00‐21  Ram Air Recovery System Special Inspections .............................................................................. 80 
11  Placards and Markings ........................................................................................................ 82 
11‐00‐00‐00  Description and Operation ........................................................................................................... 82 
11‐00‐00‐10  Interior Placards and Limitation Markings .................................................................................. 86 
11‐00‐00‐11  Exterior Placards and Markings Maintenance Practices ............................................................ 102 
12  Servicing ........................................................................................................................... 106 
12‐00‐00‐00  Description ................................................................................................................................. 106 
12‐00‐00‐20  Maintenance Practices ............................................................................................................... 106 
12‐30‐57‐20  Surface De‐Ice Boot Servicing .................................................................................................... 109 
12‐30‐61‐20  Propeller De‐Ice System Servicing .............................................................................................. 109 
12‐30‐72‐20  Ram Air Recovery System Servicing ........................................................................................... 109 
12‐32‐00‐20  Fully Enclosed High Flotation MLG Door Servicing ..................................................................... 109 
12‐50‐10‐20  Short Skirt Wing Locker Servicing ............................................................................................... 110 
Door Hinges ....................................................................................................................................................... 110 
Bayonet Latches................................................................................................................................................. 110 
Cleaning ............................................................................................................................................................. 110 
12‐50‐11‐20  Long Skirt Wing Locker Servicing ............................................................................................... 112 
Door Hinges ....................................................................................................................................................... 112 
Pin Latches ......................................................................................................................................................... 112 
Cleaning ............................................................................................................................................................. 112 
12‐53‐00‐20  Dual Aft Body Strake Servicing ................................................................................................... 114 
12‐54‐10‐20  Stainless Steel Exhaust Stack Fairing Servicing .......................................................................... 114 
12‐54‐11‐20  Composite Exhaust Stack Fairing Servicing ................................................................................ 114 
12‐57‐00‐20  Enhanced Performance Leading Edge Servicing ........................................................................ 114 
12‐61‐10‐20  Raisbeck/Hartzell Quiet Turbofan Propeller Servicing ............................................................... 114 
12‐61‐11‐20  Raisbeck/Hartzell Swept Turbofan Propeller Servicing .............................................................. 114 
12‐61‐20‐20  Raisbeck/Hartzell Quiet Turbofan Propeller Servicing ............................................................... 114 

Revision AM x
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

12‐61‐30‐20  Raisbeck/Hartzell Quiet Turbofan Propeller Servicing ............................................................... 114 
12‐61‐40‐20  Raisbeck/Hartzell Quiet Turbofan Propeller Servicing ............................................................... 114 
12‐61‐41‐20  Raisbeck/Hartzell Swept Turbofan Propeller Servicing .............................................................. 114 
12‐61‐42‐20  Raisbeck/Hartzell Five‐Blade Swept Turbofan Propeller Servicing ............................................. 115 
12‐61‐51‐20  Raisbeck/Hartzell Swept Turbofan Propeller Servicing .............................................................. 115 
12‐61‐52‐20  Raisbeck/Hartzell Five‐Blade Swept Turbofan Propeller Servicing ............................................. 115 
20  Standard Practices – Airframe ........................................................................................... 116 
20‐00‐00‐00  Description ................................................................................................................................. 116 
20‐01‐00‐00  Torque Application Information ................................................................................................. 116 
20‐02‐00‐00  Electrostatic Discharge Sensitivity Information ......................................................................... 116 
20‐03‐00‐00  Electrical Bonding Information .................................................................................................. 116 
20‐04‐00‐00  Anti‐static Coating ..................................................................................................................... 116 
20‐05‐00‐00  Fastener Locking Device Information ......................................................................................... 116 
20‐06‐00‐00  Airplane Finish Information ....................................................................................................... 116 
20‐07‐00‐00  Corrosion Control ....................................................................................................................... 116 
30  Ice and Rain Protection ..................................................................................................... 117 
Enhanced Performance Leading Edges .................................................................................................................. 117 
30‐57‐00‐00  Description and Operation ......................................................................................................... 117 
30‐57‐00‐05  Inspection ................................................................................................................................... 117 
30‐57‐00‐10  Troubleshooting ......................................................................................................................... 117 
30‐57‐00‐20  Maintenance Practices ............................................................................................................... 117 
Quiet, Swept, and Five‐Blade Swept Turbofan Propellers...................................................................................... 118 
30‐61‐00‐00  Description and Operation ......................................................................................................... 118 
30‐61‐00‐05  Inspection ................................................................................................................................... 118 
Periodic Inspection ............................................................................................................................................ 118 
Daily Checks ....................................................................................................................................................... 119 
30‐61‐00‐10  Troubleshooting ......................................................................................................................... 119 
30‐61‐00‐20  Maintenance Practices ............................................................................................................... 119 
30‐61‐10‐97  90 Series Quiet Turbofan Propellers De‐Ice Wiring .................................................................... 120 
30‐61‐11‐97  90 Series Swept Turboprop Propellers De‐Ice Wiring ................................................................. 120 
30‐61‐20‐97  F90 Series Quiet Turbofan Propellers De‐Ice Wiring Diagrams .................................................. 133 
30‐61‐30‐97  100 Series Quiet Turbofan Propellers De‐Ice Wiring Diagrams .................................................. 137 
30‐61‐40‐97  200 Series Quiet Turbofan Propellers De‐Ice Wiring Diagrams .................................................. 145 
30‐61‐41‐97  200 Series Swept Turbofan Propellers De‐Ice Wiring Diagrams ................................................ 145 
30‐61‐42‐97  200 Series Five‐Blade Swept Turbofan Propellers De‐Ice Wiring Diagrams ............................... 145 
30‐61‐50‐97  B300/B300C Quiet Turbofan Propellers De‐Ice Wiring Diagrams .............................................. 149 
30‐61‐51‐97  300/300LW, B300/B300C Four‐Blade Swept Turbofan Propellers De‐Ice Wiring Diagrams ...... 149 
30‐61‐52‐97  300/300LW, B300/B300C Five‐Blade Swept Turbofan Propellers De‐Ice Wiring Diagrams ....... 149 
Ram Air Recovery System ...................................................................................................................................... 152 
30‐72‐00‐00  Description and Operation ......................................................................................................... 152 
30‐72‐00‐05  Inspection ................................................................................................................................... 153 
Periodic Inspections ........................................................................................................................................... 153 
Daily Checks ....................................................................................................................................................... 153 
Revision AM xi
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

30‐72‐00‐10  Troubleshooting ......................................................................................................................... 156 
30‐72‐00‐20  Maintenance Practices ............................................................................................................... 157 
Repair/Replacement .......................................................................................................................................... 157 
Functional Test/adjustment .............................................................................................................................. 157 
Bypass Door Adjustment ................................................................................................................................... 157 
Particle Separator Adjustment .......................................................................................................................... 157 
32  Landing Gear ..................................................................................................................... 158 
Fully Enclosed Main Landing Gear Doors ............................................................................................................... 158 
32‐00‐00‐00  Description and Operation ......................................................................................................... 158 
32‐00‐00‐05  Inspection ................................................................................................................................... 158 
Periodic Inspections ........................................................................................................................................... 158 
Daily Checks ....................................................................................................................................................... 158 
32‐00‐00‐10  Troubleshooting ......................................................................................................................... 158 
32‐00‐00‐20  Maintenance Practices ............................................................................................................... 159 
Repair/Replacement .......................................................................................................................................... 159 
Rigging Adjustment 65‐90, 65‐A90, B90, C90, C90A, C90GT, E90 ..................................................................... 159 
Rigging Adjustment 100, A100, B100, F90, 200 Series, B300/B300C ................................................................ 159 
Functional Test 65‐90, 65‐A90, B90, C90, C90A, C90GT, E90 ............................................................................ 160 
Functional Test 100, A100, B100, F90, 200 Series, B300/B300C ....................................................................... 160 
50  Cargo and Accessory Compartments ................................................................................. 161 
Nacelle Wing Lockers ............................................................................................................................................. 161 
50‐00‐00‐00  Description and Operation ......................................................................................................... 161 
50‐00‐00‐05  Inspection ................................................................................................................................... 161 
Periodic Inspections ........................................................................................................................................... 161 
Daily Checks ....................................................................................................................................................... 161 
50‐00‐00‐20  Maintenance Practices ............................................................................................................... 162 
Short‐Skirt Wing Locker Removal ...................................................................................................................... 162 
Short‐Skirt Wing Locker Installation .................................................................................................................. 162 
Long‐Skirt Wing Locker Removal ....................................................................................................................... 162 
Long‐Skirt Wing Locker Installation ................................................................................................................... 163 
Long‐Skirt Wing Locker Removal Factory Installed on B300 ............................................................................. 163 
Long‐Skirt Wing Locker Installation Factory installed on B300 ......................................................................... 163 
Door Seal Replacement ..................................................................................................................................... 165 
Wing to Locker Seal Replacement ..................................................................................................................... 166 
Pin Latch Replacement ...................................................................................................................................... 167 
Bayonet Latch Replacement .............................................................................................................................. 168 
Bayonet and Pin Latch Receiver Adjustment ..................................................................................................... 169 
Gas Spring (85‐3520‐077) Replacement ............................................................................................................ 170 
Gas Spring (85‐3520‐098) Replacement ............................................................................................................ 170 
Wing Locker Door Hinge Replacement .............................................................................................................. 171 
51  Standard Practices and Structures ..................................................................................... 172 
51‐00‐00‐00  Description ................................................................................................................................. 172 
51‐00‐11‐00  Composite Description ............................................................................................................... 172 
51‐11‐11‐20  Wet Layup Repair Maintenance Practices ................................................................................. 172 
Materials ............................................................................................................................................................ 173 
General – Repair And Refinishing Instructions .................................................................................................. 174 
Repair Instructions for Damaged Laminated Plies ............................................................................................. 175 
Repair Instructions for Damaged Laminated Plies and Core ............................................................................. 176 
51‐12‐11‐20  Prepreg Layup Fiberglass Repair ................................................................................................ 177 

Revision AM xii
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

Materials ............................................................................................................................................................ 177 
General – Repair and Refinishing Instructions .................................................................................................. 178 
Repair Instructions for Damage of Laminated Plies .......................................................................................... 179 
Repair Instructions for Damage Laminated Ply and Core .................................................................................. 179 
51‐20‐11‐20  Repainting Fiberglass Components ............................................................................................ 182 
51‐20‐11‐23  Repainting Fiberglass Components With Anti‐Static Treatment ............................................... 183 
Surface Preparation ........................................................................................................................................... 183 
Application of Anti‐Static Coating ...................................................................................................................... 183 
Resistance Measure of Anti‐Static Coating ........................................................................................................ 184 
Top Coating ........................................................................................................................................................ 184 
53  Fuselage ........................................................................................................................... 185 
Dual Aft Body Strakes ............................................................................................................................................ 185 
53‐00‐00  Description and Operation ......................................................................................................... 185 
53‐00‐00‐05  Inspection ................................................................................................................................... 185 
Periodic Inspections ........................................................................................................................................... 185 
Daily Checks ....................................................................................................................................................... 185 
53‐00‐00‐20  Maintenance Practices ............................................................................................................... 185 
Repair/Replacement .......................................................................................................................................... 185 
54  Nacelles/Pylons ................................................................................................................ 186 
Composite and Stainless Steel Exhaust Stack Fairings ........................................................................................... 186 
54‐00‐00‐00  Description and Operation ......................................................................................................... 186 
54‐00‐00‐05  Inspection ................................................................................................................................... 186 
Periodic Inspections ........................................................................................................................................... 186 
Daily Checks ....................................................................................................................................................... 186 
54‐00‐00‐20  Maintenance Practices ............................................................................................................... 187 
Repair/Replacement .......................................................................................................................................... 187 
Composite Fairing Repair ................................................................................................................................... 187 
Stainless Steel Fairing Repair ............................................................................................................................. 187 
57  Wings ............................................................................................................................... 188 
Enhanced Performance Leading Edges .................................................................................................................. 188 
57‐00‐00‐00  Description and Operation ......................................................................................................... 188 
57‐00‐00‐05  Inspection ................................................................................................................................... 188 
Periodic Inspection ............................................................................................................................................ 188 
Daily Checks ....................................................................................................................................................... 188 
57‐00‐00‐20  Maintenance Practices ............................................................................................................... 188 
Repair/Replacement .......................................................................................................................................... 188 
Intercooler Inlet Abrasion Boot Replacement ................................................................................................... 189 
90 Series Gross Weight Increase ............................................................................................................................ 190 
57‐57‐00‐00  Description and Operation ......................................................................................................... 190 
57‐57‐00‐05  Inspections ................................................................................................................................. 190 
Periodic Inspection ............................................................................................................................................ 190 
100/A100 Series Gross Weight Increase with Quiet Turbofan Propellers .............................................................. 191 
57‐61‐30‐00  Description and Operation ......................................................................................................... 191 
57‐61‐30‐05  Inspections ................................................................................................................................. 191 
Periodic Inspection ............................................................................................................................................ 191 
Daily Checks ....................................................................................................................................................... 191 
61  Propellers ......................................................................................................................... 192 

Revision AM xiii
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

C90, E90 Series Propellers ...................................................................................................................................... 192 
61‐00‐10‐00  Quiet Turbofan Propellers Description and Operation ............................................................... 192 
61‐00‐11‐00  Swept Turbofan Propellers Description and Operation .............................................................. 193 
61‐00‐10‐05  Quiet Turbofan Propellers Inspection......................................................................................... 194 
Periodic Inspections ........................................................................................................................................... 194 
Daily Checks ....................................................................................................................................................... 194 
61‐00‐11‐05  Swept Turbofan Propellers Inspection ....................................................................................... 194 
61‐00‐00‐10  Quiet and Swept Turbofan Propellers Troubleshooting ............................................................. 195 
61‐00‐00‐20  Quiet Turbofan Propellers Maintenance Practices .................................................................... 195 
61‐00‐11‐20  Swept Turbofan Propellers Maintenance Practices ................................................................... 195 
Engine and Propeller Indicating ............................................................................................................................. 196 
61‐31‐10‐00  Description and Operation Quiet Turbofan Propellers ............................................................... 196 
61‐31‐10‐05  Inspections Quiet Turbofan Propellers ....................................................................................... 196 
61‐31‐10‐20  Maintenance Practices Quiet Turbofan Propellers .................................................................... 196 
Airspeed Indicator Range Markings ................................................................................................................... 197 
Propeller Tachometers Range Markings ............................................................................................................ 199 
Torque Meters Range Markings ........................................................................................................................ 200 
Propeller De‐Ice Ammeters Range Markings Quiet Turbofan Propellers and Swept Turbofan Propellers ....... 200 
61‐31‐11‐00  Description and Operation Swept Turbofan Propellers .............................................................. 201 
61‐31‐11‐05  Inspections Swept Turbofan Propellers ...................................................................................... 201 
61‐31‐11‐20  Maintenance Practices Swept Turbofan Propellers ................................................................... 201 
Airspeed Indicator Range Markings ................................................................................................................... 201 
Engine and Propeller Controls ............................................................................................................................... 202 
61‐76‐00‐20  Quiet Turbofan Propellers and Swept Turbofan Propellers Maintenance Practices .................. 202 
Ground Run/Low Pitch Torque Check C90, C90A, & E90 Aircraft Quiet Turbofan Propellers ........................... 203 
Ground Run/Low Pitch Torque: Blackhawk or 1,750 RPM Installations. ........................................................... 205 
Ground Run/Low Pitch Torque Check Aircraft Equipped with Raisbeck Magicam............................................ 206 
Ground Run/Low Pitch Torque Check Aircraft Equipped with Swept Turbofan Propellers .............................. 208 
Ground Run/Low Pitch Torque Check G90XT Aircraft Equipped with HC‐E4W‐3/D9290K Quiet Turbofan 
Propellers ........................................................................................................................................................... 210 
Engine Performance and Data Plate Speed Test ............................................................................................... 212 
Functional Test Magicam Adjustment Quiet Turbofan Propellers .................................................................... 214 
Low Idle Adjustment Aircraft with Magicam Quiet Turbofan Propellers .......................................................... 215 
Low Idle Adjustment Aircraft without Magicam Quiet and Swept Turbofan Propellers ................................... 215 
Takeoff RPM Quiet Turbofan Propellers and Swept Turbofan Propellers ......................................................... 215 
1,600 RPM Cruise Functional Test and Adjustment C90, C90A, C90B, and E90 Quiet Turbofan Propellers 
and Swept Turbofan Propellers ......................................................................................................................... 217 
1,600 RPM Cruise Feathering Adjustment C90, C90A, C90B, and E90 Quiet Turbofan Propellers and Swept 
Turbofan Propellers ........................................................................................................................................... 217 
Constant Speed Governor Adjustment Quiet Turbofan Propellers and Swept Turbofan Propellers ................ 217 
Constant Speed Governors adjusted from 2,200 to 1,900 MAX Takeoff RPM and 1,600 to 1,900 RPM 
Normal Operating Range ................................................................................................................................... 218 
Constant Speed Governors adjusted from 2,200 to 2,000 MAX Takeoff RPM and 1,600 to 2,000 RPM 
Normal Operating Range ................................................................................................................................... 218 
Constant Speed Governors 2,200 MAX Takeoff RPM and 1,600 to 2,200 RPM Normal Operating Range ....... 218 
Overspeed Governor Operational Test for Quiet Turbofan Propellers and Swept Turbofan Propellers .......... 220 
Reverse Not Ready Light Adjustment ................................................................................................................ 221 
Synchrophaser Target‐Screw Installation Configuration 1 ................................................................................ 222 
Synchrophaser Multiple Target Bracket Rework and Installation Configuration 2 ........................................... 222 
Synchrophaser Single Target Bracket Rework and Installation Configuration 3 ............................................... 222 

Revision AM xiv
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

Synchrophaser Target Rework and Installation Configuration 4 ....................................................................... 222 
Synchrophaser Target‐Screw Installation Configuration 5 ................................................................................ 223 
Brush Block Mounting Bracket Rework and Installation C90 Series & E90 ....................................................... 223 
Synchrophaser Magnetic Target Pickup Bracket Rework and Installation ........................................................ 223 
F90 Quiet Turbofan Propellers ............................................................................................................................... 228 
61‐00‐20‐00  Description and Operation ......................................................................................................... 228 
61‐00‐20‐05  Inspection ................................................................................................................................... 228 
Periodic Inspections ........................................................................................................................................... 228 
Daily Checks ....................................................................................................................................................... 229 
61‐00‐20‐10  Troubleshooting ......................................................................................................................... 229 
61‐00‐20‐20  Maintenance Practices ............................................................................................................... 229 
Engine and Propeller Indicating ............................................................................................................................. 230 
61‐31‐20‐00  Description and Operation ......................................................................................................... 230 
61‐31‐20‐20  Maintenance Practices ............................................................................................................... 230 
Airspeed Indicators ............................................................................................................................................ 230 
Propeller Tachometers ...................................................................................................................................... 230 
Torquemeter ...................................................................................................................................................... 230 
Ammeters .......................................................................................................................................................... 230 
Engine and Propeller Controls ............................................................................................................................... 231 
61‐76‐20‐20  Maintenance Practices ............................................................................................................... 231 
Ground Run/Low Pitch Torque Check ............................................................................................................... 231 
Low Idle Adjustment .......................................................................................................................................... 233 
High Idle Adjustment ......................................................................................................................................... 233 
Constant Speed Governors ................................................................................................................................ 233 
Overspeed Governors ........................................................................................................................................ 233 
Reversing System ............................................................................................................................................... 233 
Fuel Lever Cutoff Adjustment ............................................................................................................................ 233 
Synchrophaser Target Installation LA‐2 thru LA‐99, LA‐101 .............................................................................. 233 
Synchrophaser Target Installation LA‐100, LA‐102 thru LA‐201 ........................................................................ 233 
Brush Block Mounting Bracket Rework and Installation ................................................................................... 234 
Synchrophaser Magnetic Target Pick‐Up Bracket Rework and Installation ...................................................... 234 
100/A100 Quiet Turbofan Propellers ..................................................................................................................... 237 
61‐00‐30‐00  Description and Operation ......................................................................................................... 237 
61‐00‐30‐05  Inspection ................................................................................................................................... 238 
Inspections ......................................................................................................................................................... 238 
Daily Checks ....................................................................................................................................................... 238 
61‐00‐30‐10  Troubleshooting ......................................................................................................................... 238 
61‐00‐30‐20  Maintenance Practices ............................................................................................................... 239 
Engine and Propeller Indicating ............................................................................................................................. 239 
61‐31‐30‐00  Description and Operation ......................................................................................................... 239 
61‐31‐30‐05  Inspections ................................................................................................................................. 239 
61‐31‐30‐20  Maintenance Practices ............................................................................................................... 239 
Airspeed Indicators ............................................................................................................................................ 240 
Propeller Tachometers ...................................................................................................................................... 240 
Torque Meters ................................................................................................................................................... 240 
Propeller De‐Ice Ammeters Model 100 Only ..................................................................................................... 240 
Engine and Propeller Controls ............................................................................................................................... 241 
61‐76‐30‐20  Maintenance Practices ............................................................................................................... 241 
Ground Run Power Symmetry and Low Pitch Torque Check ............................................................................ 241 

Revision AM xv
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

Low Idle Adjustment .......................................................................................................................................... 243 
Propeller Autofeathering System (if installed) .................................................................................................. 243 
Constant Speed Governor Adjustment .............................................................................................................. 243 
Feathering Test and Adjustment ....................................................................................................................... 244 
Overspeed Governor Adjustment ...................................................................................................................... 245 
Overspeed Governor Operational Check ........................................................................................................... 245 
Reverse Not Ready Light Switch Adjustment .................................................................................................... 245 
Synchrophaser Target Installation ..................................................................................................................... 245 
Brush Block Mounting Bracket Rework and Installation ................................................................................... 246 
Synchrophaser Magnetic Target Pick‐up Bracket Rework and Installation ....................................................... 246 
61‐76‐30‐97  Engine and Propeller Controls Wiring ........................................................................................ 248 
Low Pitch Solenoid A100 Only ........................................................................................................................... 248 
Low Pitch Indicator Switch A100 Only ............................................................................................................... 248 
Low Pitch Proximity Switch A100 Only .............................................................................................................. 248 
Super King Air 200 Series Propellers ...................................................................................................................... 252 
61‐00‐40‐00  Quiet Turbofan Propellers Description and Operation ............................................................... 252 
61‐00‐41‐00  Swept Turbofan Propellers Description and Operation .............................................................. 252 
61‐00‐42‐00  Five‐Blade Swept Turbofan Propellers Description and Operation ............................................ 253 
61‐00‐40‐05  Quiet Turbofan Propellers Inspection......................................................................................... 253 
Periodic Inspections ........................................................................................................................................... 253 
Daily Checks ....................................................................................................................................................... 253 
61‐00‐41‐05  Swept Turbofan Propellers Inspection ....................................................................................... 254 
61‐00‐42‐05  Five‐Blade Swept Turbofan Propellers Inspection ...................................................................... 254 
61‐00‐40‐10  Quiet Turbofan Propellers Troubleshooting ............................................................................... 254 
61‐00‐41‐10  Swept Turbofan Propellers Troubleshooting .............................................................................. 254 
61‐00‐42‐10  Five‐Blade Swept Turbofan Propellers Troubleshooting ............................................................ 254 
61‐00‐40‐20  Quiet Turbofan Propellers Maintenance Practices .................................................................... 254 
61‐00‐41‐20  Swept Turbofan Propellers Maintenance Practices ................................................................... 255 
61‐00‐42‐20  Five‐Blade Swept Turbofan Propellers Maintenance Practices .................................................. 255 
Flight Controls Swept Turbofan Propellers ............................................................................................................ 256 
61‐27‐40‐05  Flight Controls Inspection Quiet Turbofan Propellers ................................................................ 256 
61‐27‐41‐05  Flight Controls Inspections Swept Turbofan Propellers .............................................................. 256 
61‐27‐42‐05  Flight Controls Inspections Five‐Blade Swept Turbofan Propellers ............................................ 256 
61‐27‐40‐20  Flight Controls Maintenance Practices Quiet Turbofan Propellers ............................................ 256 
61‐27‐41‐20  Flight Controls Maintenance Practices Swept Turbofan Propellers ........................................... 256 
61‐27‐42‐20  Flight Controls Maintenance Practices Five‐Blade Swept Turbofan Propellers .......................... 257 
Engine and Propeller Indicating ............................................................................................................................. 258 
61‐31‐40‐00  Description and Operation Quiet Turbofan Propellers ............................................................... 258 
61‐31‐41‐00  Description and Operation Swept Turbofan Propellers .............................................................. 258 
61‐31‐42‐00  Description and Operation Five‐Blade Swept Turbofan Propellers ............................................ 258 
61‐31‐40‐05  Inspections Quiet Turbofan Propellers ....................................................................................... 258 
61‐31‐41‐05  Inspections Swept Turbofan Propellers ...................................................................................... 258 
61‐31‐42‐05  Inspections Five‐Blade Swept Turbofan Propellers .................................................................... 258 
61‐31‐40‐20  Maintenance Practices Quiet Turbofan Propellers .................................................................... 258 
Airspeed Indicators Aircraft equipped with Rockwell Collins Pro Line 21 ......................................................... 259 
Airspeed Indicators ............................................................................................................................................ 260 

Revision AM xvi
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

Propeller Tachometers ...................................................................................................................................... 260 
Torque meters ................................................................................................................................................... 260 
Ammeters .......................................................................................................................................................... 260 
61‐31‐41‐20  Maintenance Practices Swept Turbofan Propellers ................................................................... 260 
61‐31‐42‐20  Maintenance Practices Five‐Blade Swept Turbofan Propellers .................................................. 261 
Aircraft Equipped with Rockwell Collins Pro Line 21 – OEM ............................................................................. 261 
Aircraft Equipped with Rockwell Collins Pro Line 21 – Aftermarket.................................................................. 262 
Aircraft Equipped with Rockwell Collins Pro Line Fusion – OEM ....................................................................... 263 
Aircraft Equipped with Rockwell Collins Pro Line Fusion – Aftermarket ........................................................... 263 
Aircraft Equipped with Garmin International G1000 ........................................................................................ 263 
Model 200 and A200 Series Airspeed Indicator Rework ................................................................................... 263 
Model B200 Series Airspeed Indicator Rework ................................................................................................. 264 
Propeller Ammeter Rework/Replacement ........................................................................................................ 264 
Engine and Propeller Controls ............................................................................................................................... 265 
61‐76‐40‐20  Maintenance Practices Quiet Turbofan Propellers .................................................................... 265 
Ground Run Power Symmetry and Low Pitch Torque Check ............................................................................ 265 
Low Idle Adjustment .......................................................................................................................................... 268 
Constant Speed Governor Adjustment .............................................................................................................. 268 
Overspeed Governor Operational Test.............................................................................................................. 268 
Feathering Adjustment ...................................................................................................................................... 268 
Synchrophaser Target Screw Installation .......................................................................................................... 269 
Synchrophaser Single Target Installation .......................................................................................................... 269 
Synchrophaser Multiple Target Installation ...................................................................................................... 270 
De‐Ice Brush Block Bracket Rework and Installation ......................................................................................... 271 
Synchrophaser and Dynamic Balancing Pick‐up Bracket Rework and Installation ............................................ 271 
61‐76‐41‐20  Maintenance Practices Swept Turbofan Propellers ................................................................... 276 
61‐76‐42‐20  Maintenance Practices Five‐Blade Swept Turbofan Propellers .................................................. 276 
Power Symmetry and Low Pitch Torque Check ................................................................................................. 276 
Low Idle Check ................................................................................................................................................... 279 
High Idle Check .................................................................................................................................................. 279 
Fuel Cutoff Lever Adjustment ............................................................................................................................ 279 
Propeller Autofeathering System Check ............................................................................................................ 279 
Governor Operational Check ............................................................................................................................. 279 
Propeller Synchrophaser Functional Check ....................................................................................................... 280 
synchrophaser Target and Pick‐Up Installation ................................................................................................. 280 
Type I Synchrophaser Targets ............................................................................................................................ 280 
Type II Synchrophaser Target and Balance Weight ........................................................................................... 280 
Propeller De‐Ice Brush Block Bracket Installation ............................................................................................. 280 
Synchrophaser Pick‐Up Installation ................................................................................................................... 281 
Propeller Brush Block Installation ...................................................................................................................... 281 
Metal Oxide Varistor (MOV) Module Installation .............................................................................................. 281 
Super King Air 300/300LW, B300/B300C Propellers .............................................................................................. 286 
61‐00‐51‐00  Four‐Blade Swept Turbofan Propellers Description and Operation ........................................... 286 
61‐00‐51‐05  Four‐Blade Swept Turbofan Propellers Inspection ..................................................................... 287 
Periodic Inspections ........................................................................................................................................... 287 
Daily Checks ....................................................................................................................................................... 287 
61‐00‐51‐10  Four‐Blade Swept Turbofan Propellers Checks and Fault Isolation ............................................ 288 
Power Symmetry and Low Pitch Torque Check ................................................................................................. 288 
Low Idle Check ................................................................................................................................................... 292 
Dead Band Check ............................................................................................................................................... 292 
High Idle Check .................................................................................................................................................. 292 
Maximum Reverse Check .................................................................................................................................. 293 

Revision AM xvii
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

Power Lever Mismatch Check ........................................................................................................................... 293 
Governing RPM Check ....................................................................................................................................... 293 
Solenoid Release Check ..................................................................................................................................... 293 
Ground Solenoid Check ..................................................................................................................................... 293 
Beta Valve Adjustment Check ............................................................................................................................ 293 
Low Pitch Warning Check .................................................................................................................................. 293 
Maximum Power Check ..................................................................................................................................... 293 
Propeller Synchrophaser Functional Check ....................................................................................................... 294 
Continuity Check ................................................................................................................................................ 294 
Governor Operational Check ............................................................................................................................. 295 
Pick‐Up Output Check ........................................................................................................................................ 296 
61‐00‐51‐20  Four‐Blade Swept Turbofan Propellers Maintenance Practices ................................................. 300 
Propeller Removal and Installation ................................................................................................................... 300 
Propeller De‐Ice and Synchrophaser System Bracketry Installation ................................................................. 300 
Synchrophaser Target Installation ..................................................................................................................... 300 
Synchrophaser Pick‐Up Installation ................................................................................................................... 301 
Propeller Balancing ............................................................................................................................................ 301 
Propeller Controls Nominal Setting ....................................................................................................................... 302 
Beta Arm Clevis Nominal Setting ....................................................................................................................... 302 
Beta Valve Nominal Setting ............................................................................................................................... 302 
Nf Link Nominal Setting ..................................................................................................................................... 302 
Ground Fine Solenoid Nominal Setting ............................................................................................................. 302 
61‐30‐51‐20  Four‐Blade Swept Turbofan Propellers De‐Icing System Maintenance Practices ...................... 307 
61‐00‐52‐00  Five‐Blade Swept Turbofan Propellers Description and Operation ............................................ 307 
61‐00‐52‐05  Five‐Blade Swept Turbofan Propellers Inspection ...................................................................... 307 
Periodic Inspections ........................................................................................................................................... 307 
Daily Checks ....................................................................................................................................................... 307 
61‐00‐52‐10  Five‐Blade Swept Turbofan Propellers Checks and Fault Isolation ............................................. 308 
Power Symmetry and Low Pitch Torque Check ................................................................................................. 308 
Low Idle Check ................................................................................................................................................... 312 
Dead Band Check ............................................................................................................................................... 312 
High Idle Check .................................................................................................................................................. 312 
Maximum Reverse Check .................................................................................................................................. 313 
Power Lever Mismatch Check ........................................................................................................................... 313 
Governing RPM Check ....................................................................................................................................... 313 
Solenoid Release Check ..................................................................................................................................... 313 
Ground Solenoid Check ..................................................................................................................................... 313 
Beta Valve Adjustment Check ............................................................................................................................ 313 
Low Pitch Warning Check .................................................................................................................................. 313 
Maximum Power Check ..................................................................................................................................... 313 
Propeller Synchrophaser Functional Check ....................................................................................................... 314 
Continuity Check ................................................................................................................................................ 314 
Governor Operational Check ............................................................................................................................. 315 
Pick‐Up Output Check ........................................................................................................................................ 316 
61‐00‐52‐20  Five‐Blade Swept Turbofan Propellers Maintenance Practices .................................................. 320 
Propeller Removal and Installation ........................................................................................................................ 320 
Propeller De‐Ice and Synchrophaser System Bracketry Installation ...................................................................... 320 
Synchrophaser Target Installation ......................................................................................................................... 321 
Synchrophaser Pick‐Up Installation ....................................................................................................................... 322 
Single or Dual Pick‐Up Installation ..................................................................................................................... 322 
Propeller Controls Nominal Setting ....................................................................................................................... 323 
Beta Arm Clevis Nominal Setting ....................................................................................................................... 323 

Revision AM xviii
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

Beta Valve Nominal Setting ............................................................................................................................... 323 
Nf Link Nominal Setting ...................................................................................................................................... 323 
Ground Fine Solenoid Nominal Setting ............................................................................................................. 323 
Propeller Balancing ................................................................................................................................................ 323 
61‐30‐52‐20  Five‐Blade Swept Turbofan Propellers Maintenance De‐Ice Practices ....................................... 328 
Five‐Blade Swept Turbofan Propellers Indicating .................................................................................................. 328 
61‐31‐52‐00  Description and Operation ......................................................................................................... 328 
61‐31‐52‐05  Inspections ................................................................................................................................. 328 
61‐31‐52‐20  Airspeed Indicator Rangemarking ............................................................................................. 328 
300/300LW Equipped with Rockwell Collins’ Pro Line 2 ................................................................................... 328 
300/300LW Equipped with Rockwell Collins’ Pro Line 21 ................................................................................. 328 
300/300LW Equipped with Rockwell Collins’ Fusion ......................................................................................... 328 
300/300LW Equipped with Garmin’s G1000 ..................................................................................................... 328 
B300/B300C Equipped with Rockwell Collins’ Pro Line 2 .................................................................................. 328 
B300/B300C Equipped with Rockwell Collins’ Pro Line 21 ................................................................................ 328 
B300/B300C Equipped with Rockwell Collins’ Fusion ........................................................................................ 328 
B300/B300C Equipped with Gamin’s G1000 ..................................................................................................... 328 
 

Revision AM xix
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

00 Chapter Descriptions
04 Airworthiness Limitations
This chapter details:
Mandatory modifications, replacement and structural inspection requirements for the airframe and
propellers, mandatory replacement time, inspection intervals; and procedures for fuel tanks.
Mandatory replacement time for Electrical Wiring Interconnect System (EWIS) components, limits of
validity of engineering data for structural maintenance, and instructions for continued airworthiness.

05 Time Limits/Maintenance Checks

This chapter contains the minimum requirements for Continued Airworthiness (ICA) for all Raisbeck
Systems as installed on all Beechcraft King Air Series aircraft. Maintenance checks shall be
concurrent with the existing Beechcraft Time Limits and Maintenance Checks including the allowable
time tolerances between checks as described in the applicable King Air Maintenance Manual,
Chapter 05.
Additionally, those operators under the Beechcraft Super King Air 200 Series High Utility Inspection
Program (HUIP) will find provisions that coincide with this program.
Daily Checks are intended as preflight checks for pilots and/or technicians. Daily Checks are not
intended to require a logbook entry. All other periodic inspections are intended for technician’s entry
in the logbook or other appropriate documentation.

11 Placards
This chapter details all interior and exterior placards associated with Raisbeck Systems.

12 Servicing
This chapter details general servicing of Raisbeck Systems.

20 Standard Practices Airframe

This chapter details standard maintenance practices to maintain the aircraft in airworthy condition.

30 Ice and Rain Protection

This chapter details maintenance practices for the ice protection systems on Raisbeck Enhanced
Performance Leading Edges, Ram Air Recovery System, and Raisbeck/Hartzell Propeller Systems.

32 Landing Gear
This chapter details maintenance practices for Raisbeck Fully Enclosed Main Landing Gear Doors on
aircraft equipped with high floatation landing gear.

50 Cargo and Accessory Compartments

This chapter details maintenance practices for Raisbeck Nacelle Wing Lockers and Crown Wing
Lockers.

Revision AM 1
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

51 Standard Practices Structures

This chapter provides information for acceptable repairs and repair limits on Raisbeck Systems for
composite, metallic, and formed components. In general, the repair methods used on all Raisbeck
Systems may be accomplished in accordance with AC43.13-1() Aircraft Inspection and Repair
Manual and AC43.13-2 Aircraft Alterations Manual. The repair information is recommended in
addition to the information given in AC 43.13-1() and AC 43.13-2.

53 Fuselage
This chapter details maintenance practices for Raisbeck Dual Aft Body Strakes.

54 Nacelles/Pylons
This chapter details maintenance practices for Raisbeck Composite Exhaust Stack Fairings and
Stainless Steel Exhaust Stack Fairings.

57 Wings
This chapter details maintenance practices for Raisbeck Enhanced Performance Leading Edges.

61 Propellers
This chapter details maintenance practices on Raisbeck/Hartzell Propeller Systems.

Revision AM 2
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

04 Airworthiness Limitations
04-00-00-01 Mandatory Modification, Replacement, and Structural
Inspection for Airframe Systems
There are no mandatory modification or replacement intervals on any Raisbeck Engineering King Air
airframe systems.

04-61-00-01 Mandatory Modification, Replacement, and Structural

Inspection for Propellers
Maintain Raisbeck/Hartzell Quiet Turbofan, Swept Turbofan Propellers, or Five-Blade Swept
Turbofan Propellers in accordance with the applicable Hartzell Propeller Owner’s Manual and
Logbook, Composite Propeller Blade Field Maintenance and Minor Repair Manual, and the applicable
Beechcraft King Air Maintenance Manual.

04-00-00-02 Mandatory Replacement Time, Inspection Intervals, and

Procedures for Fuel Tanks
There are no Raisbeck Engineering King Air systems that effect any existing fuel tank airworthiness
requirements.

04-00-00-03 Mandatory Replacement Time for EWIS Components

There are no EWIS components associated with any Raisbeck Engineering King Air system.

04-00-00-04 Limits of Validity of Engineering Data for Structural

Maintenance
There are no time or cycle limited components on any Raisbeck Engineering King Air airframe
systems. Components are repaired or replaced when inspection or performance of items reveals a
potentially unsafe condition or performance degradation.
Airworthiness Limitations are stipulated in the applicable Hartzell Propeller Owner’s Manual and
Logbook for time and cycle limited components of Raisbeck/Hartzell propellers.

04-00-00-05 Instructions for Continued Airworthiness

The Airworthiness Limitations section is FAA approved and specifies maintenance required under
§43.16 and §91.403 of the Federal Aviation Regulations, unless an alternative program has been
FAA approved.

Revision AM 3
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05 Time Limit/Maintenance Checks

05-00-00-00 Description
This chapter contains the minimum requirements for Continued Airworthiness (ICA) for all Raisbeck
Systems as installed on all Beechcraft King Air aircraft. Maintenance checks shall be concurrent with
the existing Beechcraft Time Limits and Maintenance Checks including the allowable time tolerances
between checks as described in the applicable King Air Maintenance Manual, Chapter 05.

05-20-00-00 Scheduled Inspection

Daily Checks, Scheduled Inspection Program (Phase Inspection), Fusion Inspection Program
(Detailed Inspection), High Utility Inspection Program (HUIP), Alternate Phase Inspection, and
Biennial Inspection requirements are set forth in this document for individual Raisbeck and
Raisbeck/Hartzell Systems. Inspections are to be accomplished in concurrence with the applicable
Beechcraft King Air Inspection Program time limit and calendar month requirements.
Aircraft structure and components should be sufficiently clean to allow for effective inspection.
Inspections should be performed to a degree to ensure systems and components will remain
serviceable until the next applicable inspection is performed. Ensure that all placards and markings
are in place and legible, especially those listed in the limitations sections of the Airplane Flight Manual
Supplement.

Revision AM 4
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

Daily Checks
Daily Checks are intended as preflight checks for pilots and/or technicians. Daily Checks are not
intended to require a logbook entry. All other Scheduled Inspections are intended for technician’s
entry in the logbook or other appropriate documentation.
Daily Inspection References

ATA
SYSTEM
REFERENCE

Ram Air Recovery System 30-72-00-05

Fully Enclosed Main Landing Gear Doors 32-00-00-05

Nacelle/Crown Wing Lockers 50-00-00-05

Dual Aft Body Strakes 53-00-00-05

Enhanced Performance Leading Edges 57-00-00-05

90 Series Quiet Turbofan Propellers 61-00-10-05

90 Series Swept Turbofan Propellers 61-00-11-05

F90 Quiet Turbofan Propellers 61-00-20-05

100 Series Quiet Turbofan Propellers 61-00-30-05

200 Series Quiet Turbofan Propellers 61-00-40-05

200 Series Swept Turbofan Propellers 61-00-41-05

200 Series Five-Blade Swept Turbofan Propellers 61-00-42-05

300/300LW and B300/B300C Four-Blade Swept 61-00-51-05

Turbofan Propellers

300/300LW and B300/B300C Five-Blade Swept 61-00-52-05

Turbofan Propellers

Revision AM 5
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

Phase Inspections
The Beechcraft King Air Phase Inspection Program, for all King Air models, is divided into four (4),
200 hour Phase Inspections. A Complete Inspection cycle is 800 hours or 24 calendar months. Each
consecutive Phase Inspection is accomplished after the previous Phase Inspection. All Special
Inspection and Unscheduled Maintenance Checks shall be accomplished independently of the Phase
Inspection Program as required. Reference Chapter 05-21-00-00 of this manual.
To facilitate scheduling Phase Inspections, Raisbeck Engineering authorizes the inspection interval
tolerances to coincide with the owner’s/operator’s approved maintenance program.

NOTE: Tolerances specified by suppliers, manufactures, DOT regulation, or FAA

regulation take precedence over inspection interval tolerances authorized by
Raisbeck Engineering. Tolerances do not accumulate.

Phase Inspection References

ATA
INSPECTION HOURS
REFERENCE

Phase 1 200 05-20-00-01

Phase 2 400 05-20-00-02

Phase 3 600 05-20-00-03

Phase 4 800 05-20-00-04

NOTE: The Phase 1 through Phase 4 Inspection Checklists includes inspection

items for all Raisbeck, Raisbeck/Hartzell Systems available for all Beechcraft
King Air Models. Some Raisbeck and Raisbeck/Hartzell Systems may not
be applicable to airframe or engine being inspected. Inspect systems as
applicable to engine or airframe.

Revision AM 6
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

Fusion Inspections
The Beechcraft King Air Fusion Inspection Program, for King Air Fusion models, is divided into four
(4) 200 hour Detailed Inspections. A complete inspection cycle is 800 hours or 48 calendar months.
Each consecutive Detailed Inspection is accomplished after the previous Detailed Inspection. All
Special Inspection and Unscheduled Maintenance Checks shall be accomplished independently of
the Detailed Inspection Program as required. Reference Chapter 05-21-00-00 of this manual.
To facilitate scheduling Fusion Inspections, Raisbeck Engineering authorizes the inspection interval
tolerances to coincide with owner’s/operator’s approved maintenance program.

NOTE: Tolerances specified by suppliers, manufactures, DOT regulation, or FAA

regulation take precedence over inspection interval tolerances authorized by
Raisbeck Engineering. Tolerances do not accumulate.

Fusion Inspection References

ATA
INSPECTION
REFERENCE

Detailed 1 05-20-00-01

Detailed 2 05-20-00-02

Detailed 3 05-20-00-03

Detailed 4 05-20-00-04

NOTE: The Detailed 1 through Detailed 4 Inspection Checklists includes inspection

items for all Raisbeck, Raisbeck/Hartzell Systems available for all Beechcraft
King Air Models. Some Raisbeck and Raisbeck/Hartzell Systems may not
be applicable to airframe or engine being inspected. Inspect systems as
applicable to engine or airframe.

Revision AM 7
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

HUIP Inspections
Only Beechcraft Super King Air 200 Series aircraft operated for a minimum of 400 hours per year are
eligible for the HUIP.

Transition from the Phase Inspection Program to the HUIP shall be accomplished upon completion of
a complete Phase Inspection Cycle or complete Phase 1 through Phase 4 Inspections. Use the flight
hours and date of the completion of Phase 4 inspection, or complete Phase 1 through Phase 4
Inspections, to establish the correct time for the Routine and Detailed Inspections of the HUIP.

The HUIP, for Beechcraft Super King Air 200 Series are divided into eight (8) inspections, four (4)
Routine Inspections starting at 200 hours, and repeating every 400 hours, alternated with four (4)
Detailed Inspections, starting at 400 hours and repeating every 400 hours. Special Inspection Items
and Unscheduled Maintenance Checks shall be accomplished independently of the HUIP as
required. Reference Chapter 05-21-00-00 of this manual.

To facilitate scheduling Routine and Detailed Inspections, Raisbeck Engineering authorizes the
inspection interval tolerances to coincide with the owner’s/operator’s approved maintenance program.

NOTE: Tolerances specified by suppliers, manufacturers, DOT regulation, or FAA

regulation take precedence over inspection interval tolerances authorized by
Raisbeck Engineering. Tolerances do not accumulate.
HUIP References

ATA
INSPECTION
REFERENCE

Routine 1 through Routine 4 05-20-00-05

Detailed 1 through Detail 4 05-20-00-06

NOTE: The Routine and Detailed Inspection Checklists include inspection items for
all Raisbeck, Raisbeck/Hartzell Systems available for Beechcraft Super King
Air 200 Series. Some Raisbeck and Raisbeck/Hartzell Systems may not be
applicable to the airframe or propeller being inspected. Inspect systems as
applicable to airframe or propeller.

Revision AM 8
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

Alternate Phase Inspections

The Beechcraft King Air Alternate Phase Inspection Program for all King Air models, is for operators
flying more than 200 hours but less than 400 hours in 24 months. All Special Inspection and
Unscheduled Maintenance Checks shall be accomplished independently of the Alternate Phase
Inspection Program as required.
Perform scheduled Phase Inspections, Phase 1 and Phase 2, together within 12 months after the
latest inspection. Perform scheduled Phase Inspections, Phase 3 and Phase 4, together within 12
months after completing the Phase 1 and Phase 2 Inspections.

ATA
INSPECTION HOURS
REFERENCE

Phase 1 & 2 200 05-20-00-02

05-20-00-02

Phase 3 & 4 400 05-20-00-03

10-20-00-04

To facilitate scheduling Alternate Phase Inspections, Raisbeck Engineering authorizes the inspection
interval tolerances to coincide with the owner’s/operator’s approved maintenance program. Raisbeck
Engineering recommends that no aircraft exceed 12 months or 200 ±20 flight hours without
completing at least one Phase Inspection. Should an aircraft exceed the limitations of the Alternate
Phase Inspection, the aircraft must complete Phase 1, Phase 2, Phase 3, and Phase 4 Inspections,
or a Complete Inspection to reestablish the aircraft’s inspection cycle.

NOTE: Tolerances specified by suppliers, manufactures, DOT regulation, or FAA

regulation take precedence over inspection interval tolerances authorized by
Raisbeck Engineering. Tolerances do not accumulate.
Biennial Inspections
The Beechcraft King Air Biennial Inspection Program for all King Air models, is for operators flying
less than 200 hours in 24 months is comprised of an Interim Inspection and a Complete Inspection.
An Interim Inspection must be completed at 12 months and every 24 months thereafter. A Complete
Inspection must be completed at 24 months and every 24 months thereafter.

ATA
INSPECTION MONTHS
REFERENCE

Interim 12 Months 05-20-00-07

Complete 24 Months 05-20-00-07

Revision AM 9
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

Daily Checklist
Daily Checklist

ATA
SYSTEM
REFERENCE

A. RAM AIR RECOVERY SYSTEM LH 30-00-00-00

1. No daily checks. N/A

B. RAM AIR RECOVERY SYSTEM RH 30-00-00-00

1. No daily checks. N/A

C. FULLY ENCLOSED MAIN LANDING GEAR DOORS LH 32-00-00-00

1. Examine doors and hinges for condition and security. 32-00-00-05

2. Examine actuating mechanisms for condition and security. 32-00-00-05

D. FULLY ENCLOSED MAIN LANDING GEAR DOORS RH 32-00-00-00

1. Examine doors and hinges for condition and security. 32-00-00-05

2. Examine actuating mechanisms for condition and security. 32-00-00-05

E. NACELLE/CROWN WING LOCKERS LH 50-00-00-00

1. Examine locker for condition and security. 50-00-00-05

2. Examine flap fairing for condition and security. 50-00-00-05

3. Ensure door is closed and latched before flight. 50-00-00-05

F. NACELLE/CROWN WING LOCKERS RH 50-00-00-00

1. Examine locker for condition and security. 50-00-00-05

2. Examine flap fairing for condition and security. 50-00-00-05

3. Ensure door is closed and latched before flight. 50-00-00-05

G. DUAL AFT BODY STRAKES LH 53-00-00-00

1. Examine strake for condition and security. 53-00-00-05

2. Examine drain holes for and clear obstructions. 53-00-00-05

H. DUAL AFT BODY STRAKES RH 53-00-00-00

1. Examine strake for condition and security. 53-00-00-05

2. Examine drain holes for and clear obstructions. 53-00-00-05

Revision AM 10
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

Daily Checklist (Continued)

ATA
SYSTEM
REFERENCE

I. EXHAUST FAIRING LH 54-00-00-00

1. Examine fairing for condition and security. 54-00-00-05

J. EXHAUST FAIRING RH 54-00-00-00

1. Examine fairing for condition and security. 54-00-00-05

K. ENHANCED PERFORMANCE LEADING EDGES LH 57-00-00-00

1. Examine the leading and wing to body fairing for condition and security. 57-00-00-05

2. Examine de-ice boot for condition and security. 57-00-00-05

L. ENHANCED PERFORMANCE LEADING EDGES RH 57-00-00-00

1. Examine the leading and wing to body fairing for condition and security. 57-00-00-05

2. Examine de-ice boot for condition and security. 57-00-00-05

M. OUTBOARD WING LH 57-00-00-00

100 SERIES ONLY, B-2 THRU B-89 WITH GROSS WEIGHT INCREASE

1. Examine ballast weight for condition and security. 57-61-30-05

N. OUTBOARD WING RH 57-00-00-00

100 SERIES ONLY, B-2 THRU B-89 WITH GROSS WEIGHT INCREASE

1. Examine ballast weight for condition and security. 57-61-30-05

Revision AM 11
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

Daily Checklist (Continued)

ATA
SYSTEM
REFERENCE

O. PROPELLERS LH 61-00-XX*-00
*Use appropriate Subject for aircraft Model and blade design.

90 Series Quiet Turbofan Propellers 61-00-10-05

90 Series Swept Turbofan Propellers 61-00-11-05

F90 Quiet Turbofan Propellers 61-00-20-05

100 Series Quiet Turbofan Propellers 61-00-30-05

200 Series Quiet Turbofan Propellers 61-00-40-05

200 Series Swept Turbofan Propellers 61-00-41-05

200 Series Five-Blade Swept Turbofan Propellers 61-00-42-05

300/300LW, B300/B300C Four-Blade Swept Turbofan Propellers 61-00-51-05

300/300LW, B300/B300C Five-Blade Swept Turbofan Propellers 61-00-52-05

1. Examine spinner and blades for condition and security. 61-00-XX*-05

2. Examine de-ice boots for condition and security. 30-61-XX*-05

P. PROPELLERS RH 61-00-XX*-00
*Use appropriate Subject for aircraft Model and blade design.

90 Series Quiet Turbofan Propellers 61-00-10-05

90 Series Swept Turbofan Propellers 61-00-11-05

F90 Quiet Turbofan Propellers 61-00-20-05

100 Series Quiet Turbofan Propellers 61-00-30-05

200 Series Quiet Turbofan Propellers 61-00-40-05

200 Series Swept Turbofan Propellers 61-00-41-05

200 Series Five-Blade Swept Turbofan Propellers 61-00-42-05

300/300LW, B300/B300C Four-Blade Swept Turbofan Propellers 61-00-51-05

300/300LW, B300/B300C Five-Blade Swept Turbofan Propellers 61-00-52-05

1. Examine spinner and blades for condition and security. 61-00-XX*-05

2. Examine de-ice boots for condition and security. 30-61-XX*-05

Revision AM 12
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-01 Scheduled Inspection Program Phase 1 or Detailed 1

Inspection
05-20-00-01 Phase 1 or Detailed 1 Inspection

ATA
SYSTEM MECH INSP
REFERENCE

A. RAM AIR RECOVERY SYSTEM LH 30-00-00-00 -- --

1. Examine the Diaphragm Seals for condition, 30-72-00-05

attachment, and sealing conditions.

2. Examine the Bypass Door Seals for condition, 30-72-00-05

attachment, and sealing conditions. Examine for
freedom of movement and correct adjustment.

3. Examine the Particle Separator for structural 30-72-00-05

condition and attachment. Examine for freedom of
movement and proper travel.

4. Examine the Fixed Turning Vane for structural 30-72-00-05

condition and attachment.

5. Examine the Ice Shedder Screen for condition and 30-72-00-05

attachment.

B. RAM AIR RECOVERY SYSTEM RH 30-00-00-00 -- --

1. Examine the Diaphragm Seals for condition, 30-72-00-05

attachment, and sealing conditions.

2. Examine the Bypass Door Seals for condition, 30-72-00-05

attachment, and sealing conditions. Examine for
freedom of movement and correct adjustment.

3. Examine the Particle Separator for structural 30-72-00-05

condition and attachment. Examine for freedom of
movement and proper travel.

4. Examine the Fixed Turning Vane for structural 30-72-00-05

condition and attachment.

5. Examine the Ice Shedder Screen for condition and 30-72-00-05

attachment.

Revision AM 13
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-01 Phase 1 or Detailed 1 Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

C. FULLY ENCLOSED MLG DOORS LH 32-00-00-00 -- --

1. Examine the door, hinges, and door actuating 32-00-00-05

linkage for wear, condition, and security.

D. FULLY ENCLOSED MLG DOORS RH 32-00-00-00 -- --

1. Examine the door, hinges, and door actuating 32-00-00-05

linkage for wear, condition, and security.

E. WING LOCKERS LH 50-00-00-00 -- --

1. Examine Locker Shell for condition and security. 50-00-00-05

2. Examine Locker Door for condition and security. 50-00-00-05

3. Examine Latches for condition and security. 50-00-00-05

4. Examine the Hinges for condition and security. 50-00-00-05

5. Examine Flap Fairing for condition and security of 50-00-00-05

attachment.

F. WING LOCKER RH 50-00-00-00 -- --

1. Examine Locker Shell for condition and security. 50-00-00-05

2. Examine Locker Door for condition and security. 50-00-00-05

3. Examine Latches for condition and security. 50-00-00-05

4. Examine the Hinges for condition and security. 50-00-00-05

5. Examine Flap Fairing for condition and security of 50-00-00-05

attachment.

Revision AM 14
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-01 Phase 1 or Detailed 1 Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

G. DUAL AFT BODY STRAKES LH 53-00-00-00 -- --

1. Examine Strake for condition and security. 53-00-00-05

2. Examine drain holes for obstructions. 53-00-00-05

H. DUAL AFT BODY STRAKES RH 53-00-00-00 -- --

1. Examine Strake for condition and security. 53-00-00-05

2. Examine drain holes for obstructions. 53-00-00-05

I. EXHAUST FAIRINGS LH 54-00-00-00 -- --

1. Examine Fairings for condition and security. 54-00-00-05

2. Examine fasteners for condition and security. 53-00-00-05

3. Remove Fairings and examine gasket for condition. 53-00-00-05

J. EXHAUST FAIRINGS RH 54-00-00-00 -- --

1. Examine Fairings for condition and security. 54-00-00-05

2. Examine fasteners for condition and security. 54-00-00-05

3. Remove Fairings and examine gasket for condition. 54-00-00-05

K. ENHANCED PERFORMANCE LEADING EDGE LH 57-00-00-00 -- --

1. Examine the de-ice boot for condition and security. 30-57-00-05

2. Examine the intercooler duct and gasket for 57-00-00-05

condition and security.

3. Examine the Wing-to-Body fairing for condition and 57-00-00-05

security.

4. Using Non-destructive Testing (NDT), such as a 57-00-00-05

manual tap test, examine the leading edge for
delamination. Examine both sides of core.

5. Remove the Wing-to-Body Fairing. Inspect the 57-00-00-05

fairing, leading edge, and fuselage for condition and
chafing.

6. Remove the inboard Leading Edge. Inspect the 57-00-00-05

inner surface of the leading edge for condition and
delamination. Inspect the intercooler duct for
condition.

Revision AM 15
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-01 Phase 1 or Detailed 1 Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

L. ENHANCED PERFORMANCE LEADING EDGE RH 57-00-00-00 -- --

1. Examine the de-ice boot for condition and security. 30-57-00-05

2. Examine the intercooler duct and gasket for 57-00-00-05

condition and security.

3. Examine the Wing-to-Body Fairing for condition and 57-00-00-05

security.

4. Using Non-destructive Testing (NDT), such as a 57-00-00-05

manual tap test, examine the leading edge for
delamination. Examine both sides of core.

5. Remove the Wing-to-Body Fairing. Inspect the 57-00-00-05

fairing, leading edge, and fuselage for condition and
chafing.

6. Remove the inboard Leading Edge. Inspect the 57-00-00-05

inner surface of the leading edge for condition and
delamination. Inspect the intercooler duct for
condition.

M. OUTBOARD WING LH 57-00-00-00

C90A AND C90GT ONLY LJ-1138 THRU -- --
LJ-1145 AND LJ-1147 AND AFTER WITH
OPTIONAL GROSS WEIGHT INCREASE

1. Remove the lower Wing Tip Attachment Cover, 57-57-00-05

Panel 20. Inspect the Ballast Weight and Wing Tip 57-61-10-05
Center Rib (000-170012-3) for condition and 57-61-11-05
security.
CAUTION: THE RETAINING HARDWARE IS NON-
MAGNETIC. USE OF MAGNETIC
HARDWARE CAN INTERFERE WITH
THE AIRCRAFT’S NAVIGATION
SYSTEM. IF THE BALLAST WEIGHT IS
REMOVED ENSURE IT IS REINSTALLED
USING THE CORRECT HARDWARE.

2. Re-install the Access Panel, verifying use of correct Beechcraft

hardware. King Air MM

Revision AM 16
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-01 Phase 1 or Detailed 1 Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

N. OUTBOARD WING RH 57-00-00-00

C90A AND C90GT ONLY LJ-1138 THRU -- --
LJ-1145 AND LJ-1147 AND AFTER WITH
OPTIONAL GROSS WEIGHT INCREASE

1. Remove the lower Wing Tip Attachment Cover, 57-57-00-05

Panel 20. Inspect the Ballast Weight and Wing Tip 57-61-10-05
Center Rib (000-170012-4) for condition and 57-61-11-05
security.
CAUTION: THE RETAINING HARDWARE IS NON-
MAGNETIC. USE OF MAGNETIC
HARDWARE CAN INTERFERE WITH
THE AIRCRAFT’S NAVIGATION
SYSTEM. IF THE BALLAST WEIGHT IS
REMOVED ENSURE IT IS REINSTALLED
USING THE CORRECT HARDWARE.

2. Re-install the Access Panel, verifying use of correct Beechcraft

hardware. King Air MM

O. OUTBOARD WING LH 57-00-00-00

100 SERIES ONLY, B-2 THRU B-89 & B93 WITH -- --
GROSS WEIGHT INCREASE

1. Inspect the Ballast Weight for condition and security 57-61-30-05

of attachment.
CAUTION: THE RETAINING HARDWARE IS NON-
MAGNETIC. USE OF MAGNETIC
HARDWARE CAN INTERFERE WITH
THE AIRCRAFT’S NAVIGATION
SYSTEM. IF THE BALLAST WEIGHT IS
REMOVED ENSURE IT IS REINSTALLED
USING THE CORRECT HARDWARE.

P. OUTBOARD WING RH 57-00-00-00

100 SERIES ONLY, B-2 THRU B-89 & B93 WITH -- --
GROSS WEIGHT INCREASE

1. Inspect the Ballast Weight for condition and security 57-61-30-05

of attachment.
CAUTION: THE RETAINING HARDWARE IS NON-
MAGNETIC. USE OF MAGNETIC
HARDWARE CAN INTERFERE WITH
THE AIRCRAFT’S NAVIGATION
SYSTEM. IF THE BALLAST WEIGHT IS
REMOVED ENSURE IT IS REINSTALLED
USING THE CORRECT HARDWARE.

Revision AM 17
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-01 Phase 1 or Detailed 1 Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

PROPELLERS
*Use appropriate Subject for your airplane Model and
blade design. SYSTEM

61-00-XX*-00

Subject 10 90 Series Quiet Turbofan Propellers

Subject 11 90 Series Swept Turbofan Propellers

Subject 20 F90 Quiet Turbofan Propellers

Subject 30 100 Series Quiet Turbofan Propellers

Subject 40 200 Series Quiet Turbofan Propellers

Subject 41 200 Series Swept Turbofan Propellers

Subject 42 200 Series Five-Blade Swept Turbofan

Propellers

Subject 51 300/300LW, B300/B300C Four-Blade Swept

Turbofan Propellers

Subject 52 300/300LW, B300/B300C Five-Blade Swept

Turbofan Propellers

Q. PROPELLERS LH 61-00-XX*-00 -- --

1. Inspect propeller de-ice system for condition and 30-61-00-05

security (spinner removal required).

2. Inspect Propeller for condition and security. 61-00-XX*-05

R. PROPELLERS RH 61-00-XX*-00 -- --

1. Inspect propeller de-ice system for condition and 30-61-00-05

security (spinner removal required).

2. Inspect Propeller for condition and security. 61-00-XX*-05

S. ENGINE TRUSS LH 71-00-00-00

200 SERIES, 300/300LW, B300/B300C -- --
EQUIPPED WITH FIVE-BLADE SWEPT
TURBOFAN PROPELLERS

1. Inspect for cracks, dents, chafing, and corrosion. 71-00-00-05

Special attention should be made to areas around
clamps.

2. Inspect vibration isolators (mounts) for deterioration, 71-00-00-05

damage, and attachment.

Revision AM 18
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-01 Phase 1 or Detailed 1 Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

T. ENGINE TRUSS RH 71-00-00-00

200 SERIES, 300/300LW, B300/B300C -- --
EQUIPPED WITH FIVE-BLADE SWEPT
TURBOFAN PROPELLERS

1. Inspect for cracks, dents, chafing, and corrosion. 71-00-00-05

Special attention should be made to areas around
clamps.

2. Inspect vibration isolators (mounts) for deterioration, 71-00-00-05

damage, and attachment.

U. FUNCTIONAL CHECKS Beechcraft

-- --
King Air MM

1. Perform all Operational Inspection items per the Beechcraft

applicable Beechcraft King Air Maintenance Manual, King Air MM
Scheduled Inspection Program (Phase/Detailed1 &
3).

V. POST INSPECTION ITEMS -- -- --

1. Lubricate as necessary. 12-00-00-00

2. Determine that all required placards are in place and 11-00-00-00

legible.

3. Complete all necessary logbook entries. --

Revision AM 19
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-01 Phase 1 or Detailed 1 Inspection Discrepancy Sheet

05-20-00-01 Phase 1 or Detailed 1 Inspection Discrepancy Sheet

DISCREPANCY CORRECTIVE ACTION MECH INSP

Revision AM 20
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-02 Scheduled Inspection Program Phase 2 or Detailed 2

Inspection
05-20-00-02 Phase 2 or Detailed 2 Inspection

ATA
SYSTEM MECH INSP
REFERENCE

A. RAM AIR RECOVERY SYSTEM LH 30-00-00-00 -- --

1. Examine the Diaphragm Seals for condition, 30-72-00-05

attachment, and sealing conditions.

2. Examine the Bypass Door Seals for condition, 30-72-00-05

attachment, and sealing conditions. Examine for
freedom of movement and correct adjustment.

3. Examine the Particle Separator for structural 30-72-00-05

condition and attachment. Examine for freedom of
movement and proper travel.

4. Examine the Fixed Turning Vane for structural 30-72-00-05

condition and attachment.

5. Examine the Ice Shedder Screen for condition and 30-72-00-05

attachment.

B. RAM AIR RECOVERY SYSTEM RH 30-00-00-00 -- --

1 Examine the Diaphragm Seals for condition, 30-72-00-05

attachment, and sealing conditions.

2. Examine the Bypass Door Seals for condition, 30-72-00-05

attachment, and sealing conditions. Examine for
freedom of movement and correct adjustment.

3. Examine the Particle Separator for structural 30-72-00-05

condition and attachment. Examine for freedom of
movement and proper travel.

4. Examine the Fixed Turning Vane for structural 30-72-00-05

condition and attachment.

5. Examine the Ice Shedder Screen for condition and 30-72-00-05

attachment.

Revision AM 21
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-02 Phase 2 or Detailed 2 Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

C. FULLY ENCLOSED MLG DOORS LH 32-00-00-00 -- --

1. Examine the door, hinges, and door actuating 32-00-00-05

linkage for wear, condition, and security.

2. Jack aircraft per the applicable Beechcraft King Air Beechcraft

Maintenance Manual and perform a landing gear King Air MM
retraction test.

3. Examine the door retraction linkage for proper 32-00-00-20

operation and adjustment.

4. Examine the doors for proper fit and security when 32-00-00-20
the landing gear is retracted.

5. Perform a Manual/Emergency landing gear Beechcraft

extension test per the applicable Beechcraft King Air King Air MM
Maintenance Manual.

D. FULLY ENCLOSED MLG DOORS RH 32-00-00-00 -- --

1. Examine the door, hinges, and door actuating 32-00-00-05

linkage for wear, condition, and security.

2. Jack aircraft per the applicable Beechcraft King Air Beechcraft

Maintenance Manual and perform a landing gear King Air MM
retraction test.

3. Examine the door retraction linkage for proper 32-00-00-20

operation and adjustment.

4. Examine the doors for proper fit and security when 32-00-00-20
the landing gear is retracted.

5. Perform a Manual/Emergency landing gear Beechcraft

extension test per the applicable Beechcraft King Air King Air MM
Maintenance Manual.

E. WING LOCKERS LH 50-00-00-00 -- --

1. Examine Locker Shell for condition and security. 50-00-00-05

2. Examine Locker Door for condition and security. 50-00-00-05

3. Examine Latches for condition and security. 50-00-00-05

4. Examine Hinges for condition and security. 50-00-00-05

5. Examine the Flap Fairing for condition and security 50-00-00-05

of attachment.

Revision AM 22
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-02 Phase 2 or Detailed 2 Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

F. WING LOCKER RH 50-00-00-00 -- --

1. Examine Locker Shell for condition and security. 50-00-00-05

2. Examine Locker Door for condition and security. 50-00-00-05

3. Examine Latches for condition and security. 50-00-00-05

4. Examine Hinges for condition and security. 50-00-00-05

5. Inspect the Flap Fairing for condition and security of 50-00-00-05

attachment.

G. DUAL AFT BODY STRAKES LH 53-00-00-00 -- --

1. Examine Strake for condition and security. 53-00-00-05

2. Examine drain holes for obstructions. 53-00-00-05

H. DUAL AFT BODY STRAKES RH 53-00-00-00 -- --

1. Examine Strake for condition and security. 53-00-00-05

2. Examine drain holes for obstructions. 53-00-00-05

I. EXHAUST FAIRINGS LH 54-00-00-00 -- --

1. Examine Fairings for condition and security. 54-00-00-05

2. Examine fasteners for condition and security. 54-00-00-05

3. Remove Fairings and examine gasket for condition. 54-00-00-05

J. EXHAUST FAIRINGS RH 54-00-00-00 -- --

1. Examine Fairings for condition and security. 54-00-00-05

2. Examine fasteners for condition and security. 54-00-00-05

3. Remove Fairings and examine gasket for condition. 54-00-00-05

Revision AM 23
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-02 Phase 2 or Detailed 2 Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

K. ENHANCED PERFORMANCE LEADING EDGE LH 57-00-00-00 -- --

1. Examine the de-ice boot for condition and security. 30-57-00-05

2. Examine the intercooler duct and gasket for 57-00-00-05

condition and security.

3. Examine the Wing-to-Body Fairing for condition and 57-00-00-05

security.

4. Using Non-destructive Testing (NDT), such as a 57-00-00-05

manual tap test, examine the leading edge for
delamination.

L. ENHANCED PERFORMANCE LEADING EDGE RH 57-00-00-00 -- --

1. Examine the de-ice boot for condition and security. 30-57-00-05

2. Examine the intercooler duct and gasket for 57-00-00-05

condition and security.

3. Examine the Wing-to-Body Fairing for condition and 57-00-00-05

security.

4. Using Non-destructive Testing (NDT), such as a 57-00-00-05

manual tap test, examine the leading edge for
delamination.

Revision AM 24
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-02 Phase 2 or Detailed 2 Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

PROPELLERS
*Use appropriate Subject for your airplane Model and
blade design. SYSTEM

61-00-XX*-00

Subject 10 90 Series Quiet Turbofan Propellers

Subject 11 90 Series Swept Turbofan Propellers

Subject 20 F90 Quiet Turbofan Propellers

Subject 30 100 Series Quiet Turbofan Propellers

Subject 40 200 Series Quiet Turbofan Propellers

Subject 41 200 Series Swept Turbofan Propellers

200 Series Five-Blade Swept Turbofan

Subject 42
Propellers

Subject 51 300/300LW, B300/B300C Four-Blade Swept

Turbofan Propellers

Subject 52 300/300LW, B300/B300C Five-Blade Swept

Turbofan Propellers

M. PROPELLERS LH 61-00-XX*-00 -- --

1. Inspect propeller de-ice system for condition and 30-61-00-05

security (spinner removal required).

2. Inspect Propeller for condition and security. 61-00-XX*-05

N. PROPELLERS RH 61-00-XX*-00 -- --

1. Inspect Propeller de-ice system for condition and 30-61-00-05

security (spinner removal required).

2. Inspect Propeller for condition and security. 61-00-XX*-05

O. ENGINE TRUSS LH 71-00-00-00

200 SERIES, 300/300LW, B300/B300C -- --
EQUIPPED WITH FIVE-BLADE SWEPT
TURBOFAN PROPELLERS

1. Inspect for cracks, dents, chafing, and corrosion. 71-00-00-05

Special attention should be made to areas around
clamps.

2. Inspect vibration isolators (mounts) for deterioration, 71-00-00-05

damage, and attachment.

Revision AM 25
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-02 Phase 2 or Detailed 2 Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

P. ENGINE TRUSS RH 71-00-00-00

200 SERIES, 300/300LW, B300/B300C -- --
EQUIPPED WITH FIVE-BLADE SWEPT
TURBOFAN PROPELLERS

1. Inspect for cracks, dents, chafing, and corrosion. 71-00-00-05

Special attention should be made to areas around
clamps.

2. Inspect vibration isolators (mounts) for deterioration, 71-00-00-05

damage, and attachment.

Q. FUNCTIONAL CHECKS Beechcraft

-- --
King Air MM

1. Perform all Operational Inspection items per the Beechcraft

applicable Beechcraft King Air Maintenance Manual, King Air MM
Scheduled Inspection Program (Phase/Detailed 2 &
4).

R. POST INSPECTION ITEMS -- -- --

1. Lubricate as necessary. 12-00-00-00

2. Determine that all required placards are in place and 11-00-00-00

legible

3. Complete all necessary logbook entries. --

Revision AM 26
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-02 Phase 2 or Detailed 2 Inspection Discrepancy Sheet

05-20-00-02 Phase 2 or Detailed 2 Inspection Discrepancy Sheet

DISCREPANCY CORRECTIVE ACTION MECH INSP

Revision AM 27
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-03 Scheduled Inspection Program Phase 3 or Detailed 3

Inspection
05-20-00-03 Phase 3 or Detailed 3 Inspection

ATA
SYSTEM MECH INSP
REFERENCE

A. RAM AIR RECOVERY SYSTEM LH 30-00-00-00 -- --

1. Examine the Diaphragm Seals for condition, 30-72-00-05

attachment, and sealing conditions.

2. Examine the Bypass Door Seals for condition, 30-72-00-05

attachment, and sealing conditions. Examine for
freedom of movement and correct adjustment.

3. Examine the Particle Separator for structural 30-72-00-05

condition and attachment. Examine for freedom of
movement and proper travel.

4. Examine the Fixed Turning Vane for structural 30-72-00-05

condition and attachment.

5. Examine the Ice Shedder Screen for condition and 30-72-00-05

attachment.

B. RAM AIR RECOVERY SYSTEM RH 30-00-00-00 -- --

1. Examine the Diaphragm Seals for condition, 30-72-00-05

attachment, and sealing conditions.

2. Examine the Bypass Door Seals for condition, 30-72-00-05

attachment, and sealing conditions. Examine for
freedom of movement and correct adjustment.

3. Examine the Particle Separator for structural 30-72-00-05

condition and attachment. Examine for freedom of
movement and proper travel.

4. Examine the Fixed Turning Vane for structural 30-72-00-05

condition and attachment.

5. Examine the Ice Shedder Screen for condition and 30-72-00-05

attachment.

Revision AM 28
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-03 Phase 3 or Detailed 3 Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

C. FULLY ENCLOSED MLG DOORS LH 32-00-00-00 -- --

1. Examine the door, hinges, and door actuating 32-00-00-05

linkage for wear, condition, and security.

D. FULLY ENCLOSED MLG DOORS RH 32-00-00-00 -- --

1. Examine the door, hinges, and door actuating 32-00-00-05

linkage for wear, condition, and security.

E. WING LOCKERS LH 50-00-00-00 -- --

1. Examine Locker Shell for condition and security. 50-00-00-05

2. Examine Locker Door for condition and security. 50-00-00-05

3. Examine Latches for condition and security. 50-00-00-05

4. Examine the Hinges for condition and security. 50-00-00-05

5. Examine Flap Fairing for condition and security of 50-00-00-05

attachment.

F. WING LOCKER RH 50-00-00-00 -- --

1. Examine Locker Shell for condition and security. 50-00-00-05

2. Examine Locker Door for condition and security. 50-00-00-05

3. Examine Latches for condition and security. 50-00-00-05

4. Examine the Hinges for condition and security. 50-00-00-05

5. Examine Flap Fairing for condition and security of 50-00-00-05

attachment.

Revision AM 29
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-03 Phase 3 or Detailed 3 Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

G. DUAL AFT BODY STRAKES LH 53-00-00-00 -- --

1. Examine Strake for condition and security. 53-00-00-05

2. Examine drain holes for obstructions. 53-00-00-05

H. DUAL AFT BODY STRAKES RH 53-00-00-00 -- --

1. Examine Strake for condition and security. 53-00-00-05

2. Examine drain holes for obstructions. 53-00-00-05

I. EXHAUST FAIRINGS LH 54-00-00-00 -- --

1. Examine Fairings for condition and security. 54-00-00-05

2. Examine fasteners for condition and security. 53-00-00-05

3. Remove Fairings and examine gasket for condition. 53-00-00-05

J. EXHAUST FAIRINGS RH 54-00-00-00 -- --

1. Examine Fairings for condition and security. 54-00-00-05

2. Examine fasteners for condition and security. 54-00-00-05

3. Remove Fairings and examine gasket for condition. 54-00-00-05

K. ENHANCED PERFORMANCE LEADING EDGE LH 57-00-00-00 -- --

1. Examine the de-ice boot for condition and security. 30-57-00-05

2. Examine the intercooler duct and gasket for 57-00-00-05

condition and security.

3. Examine the Wing-to-Body fairing for condition and 57-00-00-05

security.

4. Using Non-destructive Testing (NDT), such as a 57-00-00-05

manual tap test, examine the leading edge for
delamination. Examine both sides of core.

5. Remove the Wing-to-Body Fairing. Inspect the 57-00-00-05

fairing, leading edge, and fuselage for condition and
chafing.

6. Remove the inboard Leading Edge. Inspect the 57-00-00-05

inner surface of the leading edge for condition and
delamination. Inspect the intercooler duct for
condition.

Revision AM 30
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-03 Phase 3 or Detailed 3 Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

L. ENHANCED PERFORMANCE LEADING EDGE RH 57-00-00-00 -- --

1. Examine the de-ice boot for condition and security. 30-57-00-05

2. Examine the intercooler duct and gasket for 57-00-00-05

condition and security.

3. Examine the Wing-to-Body Fairing for condition and 57-00-00-05

security.

4. Using Non-destructive Testing (NDT), such as a 57-00-00-05

manual tap test, examine the leading edge for
delamination. Examine both sides of core.

5. Remove the Wing-to-Body Fairing. Inspect the 57-00-00-05

fairing, leading edge, and fuselage for condition and
chafing.

6. Remove the inboard Leading Edge. Inspect the 57-00-00-05

inner surface of the leading edge for condition and
delamination. Inspect the intercooler duct for
condition.

M. OUTBOARD WING LH 57-00-00-00

C90A AND C90GT ONLY: LJ-1138 THRU -- --
LJ-1145 AND LJ-1147 AND AFTER WITH
OPTIONAL GROSS WEIGHT INCREASE

1. Remove the lower Wing Tip Attachment Cover, 57-57-00-05

Panel 20. Inspect the Ballast Weight and Wing Tip 57-61-10-05
Center Rib (000-170012-3) for condition and 57-61-11-05
security.
CAUTION: THE RETAINING HARDWARE IS NON-
MAGNETIC. USE OF MAGNETIC
HARDWARE CAN INTERFERE WITH
THE AIRCRAFT’S NAVIGATION
SYSTEM. IF THE BALLAST WEIGHT IS
REMOVED ENSURE IT IS REINSTALLED
USING THE CORRECT HARDWARE.

2. Re-install the Access Panel, verifying use of correct Beechcraft

hardware. King Air MM

Revision AM 31
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-03 Phase 3 or Detailed 3 Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

N. OUTBOARD WING RH 57-00-00-00

C90A AND C90GT ONLY: LJ-1138 THRU -- --
LJ-1145 AND LJ-1147 AND AFTER WITH
OPTIONAL GROSS WEIGHT INCREASE

1. Remove the lower Wing Tip Attachment Cover, 57-57-00-05

Panel 20. Inspect the Ballast Weight and Wing Tip 57-61-10-05
Center Rib (000-170012-4) for condition and 57-61-11-05
security.
CAUTION: THE RETAINING HARDWARE IS NON-
MAGNETIC. USE OF MAGNETIC
HARDWARE CAN INTERFERE WITH
THE AIRCRAFT’S NAVIGATION
SYSTEM. IF THE BALLAST WEIGHT IS
REMOVED ENSURE IT IS REINSTALLED
USING THE CORRECT HARDWARE.

2. Re-install the Access Panel, verifying use of correct Beechcraft

hardware. King Air MM

O. OUTBOARD WING LH 57-00-00-00

100 SERIES ONLY: B-2 THRU B-89 AND B93 -- --
WITH GROSS WEIGHT INCREASE

1. Inspect the Ballast Weight for condition and security 57-61-30-05

of attachment.
CAUTION: THE RETAINING HARDWARE IS NON-
MAGNETIC. USE OF MAGNETIC
HARDWARE CAN INTERFERE WITH
THE AIRCRAFT’S NAVIGATION
SYSTEM. IF THE BALLAST WEIGHT IS
REMOVED ENSURE IT IS REINSTALLED
USING THE CORRECT HARDWARE.

P. OUTBOARD WING RH 57-00-00-00

100 SERIES ONLY: B-2 THRU B-89 AND B93 -- --
WITH GROSS WEIGHT INCREASE

1. Inspect the Ballast Weight for condition and security 57-61-30-05

of attachment.
CAUTION: THE RETAINING HARDWARE IS NON-
MAGNETIC. USE OF MAGNETIC
HARDWARE CAN INTERFERE WITH
THE AIRCRAFT’S NAVIGATION
SYSTEM. IF THE BALLAST WEIGHT IS
REMOVED ENSURE IT IS REINSTALLED
USING THE CORRECT HARDWARE.

Revision AM 32
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-03 Phase 3 or Detailed 3 Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

PROPELLERS
*Use appropriate Subject for your airplane Model and
blade design. SYSTEM

61-00-XX*-00

Subject 10 90 Series Quiet Turbofan Propellers

Subject 11 90 Series Swept Turbofan Propellers

Subject 20 F90 Quiet Turbofan Propellers

Subject 30 100 Series Quiet Turbofan Propellers

Subject 40 200 Series Quiet Turbofan Propellers

Subject 41 200 Series Swept Turbofan Propellers

200 Series Five-Blade Swept Turbofan

Subject 42
Propellers

Subject 51 300/300LW, B300/B300C Four-Blade Swept

Turbofan Propellers

Subject 52 300/300LW, B300/B300C Five-Blade Swept

Turbofan Propellers

Q. PROPELLERS LH 61-00-XX*-00 -- --

1. Inspect propeller de-ice system for condition and 30-61-00-05

security (spinner removal required).

2. Inspect Propeller for condition and security. 61-00-XX*-05

R. PROPELLERS RH 61-00-XX*-00 -- --

1. Inspect propeller de-ice system for condition and 30-61-00-05

security (spinner removal required).

2. Inspect Propeller for condition and security. 61-00-XX*-05

Revision AM 33
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-03 Phase 3 or Detailed 3 Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

S. ENGINE TRUSS LH 71-00-00-00

200 SERIES, 300/300LW, B300/B300C -- --
EQUIPPED WITH FIVE-BLADE SWEPT
TURBOFAN PROPELLERS

1. Inspect for cracks, dents, chafing, and corrosion. 71-00-00-05

Special attention should be made to areas around
clamps.

2. Inspect vibration isolators (mounts) for deterioration, 71-00-00-05

damage, and attachment.

T. ENGINE TRUSS RH 71-00-00-00

200 SERIES, 300/300LW, B300/B300C -- --
EQUIPPED WITH FIVE-BLADE SWEPT
TURBOFAN PROPELLERS

1. Inspect for cracks, dents, chafing, and corrosion. 71-00-00-05

Special attention should be made to areas around
clamps.

2. Inspect vibration isolators (mounts) for deterioration, 71-00-00-05

damage, and attachment.

U. FUNCTIONAL CHECKS Beechcraft

-- --
King Air MM

1. Perform all Operational Inspection items per the Beechcraft

applicable Beechcraft King Air Maintenance Manual, King Air MM
Scheduled Inspection Program (Phase/Detailed 1 &
3).

V. POST INSPECTION ITEMS -- -- --

1. Lubricate as necessary. 12-00-00-00

2. Determine that all required placards are in place an 11-00-00-00

legible.

3. Complete all necessary logbook entries. --

Revision AM 34
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-03 Phase 3 or Detailed 3 Inspection Discrepancy Sheet

05-20-00-03 Phase 3 or Detailed 3 Inspection Discrepancy Sheet

DISCREPANCY CORRECTIVE ACTION MECH INSP

Revision AM 35
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-04 Scheduled Inspection Program Phase 4 or Detailed 4

Inspection
05-20-00-04 Phase 4 or Detailed 4 Inspection

ATA
SYSTEM MECH INSP
REFERENCE

A. RAM AIR RECOVERY SYSTEM LH 30-00-00-00 -- --

1. Examine the Diaphragm Seals for condition, 30-72-00-05

attachment, and sealing conditions.

2. Examine the Bypass Door Seals for condition, 30-72-00-05

attachment, and sealing conditions. Examine for
freedom of movement and correct adjustment.

3. Examine the Particle Separator for structural 30-72-00-05

condition and attachment. Examine for freedom of
movement and proper travel.

4. Examine the Fixed Turning Vane for structural 30-72-00-05

condition and attachment.

5. Examine the Ice Shedder Screen for condition and 30-72-00-05

attachment.

B. RAM AIR RECOVERY SYSTEM RH 30-00-00-00 -- --

1 Examine the Diaphragm Seals for condition, 30-72-00-05

attachment, and sealing conditions.

2. Examine the Bypass Door Seals for condition, 30-72-00-05

attachment, and sealing conditions. Examine for
freedom of movement and correct adjustment.

3. Examine the Particle Separator for structural 30-72-00-05

condition and attachment. Examine for freedom of
movement and proper travel.

4. Examine the Fixed Turning Vane for structural 30-72-00-05

condition and attachment.

5. Examine the Ice Shedder Screen for condition and 30-72-00-05

attachment.

Revision AM 36
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-04 Phase 4 or Detailed 4 Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

C. FULLY ENCLOSED MLG DOORS LH 32-00-00-00 -- --

1. Examine the door, hinges, and door actuating 32-00-00-05

linkage for wear, condition, and security.

2. Jack aircraft per the applicable Beechcraft King Air Beechcraft

Maintenance Manual and perform a landing gear King Air MM
retraction test.

3. Examine the door retraction linkage for proper 32-00-00-20

operation and adjustment.

4. Examine the doors for proper fit and security when 32-00-00-20
the landing gear is retracted.

5. Perform a Manual/Emergency landing gear Beechcraft

extension test per the applicable Beechcraft King Air King Air MM
Maintenance Manual.

D. FULLY ENCLOSED MLG DOORS RH 32-00-00-00 -- --

1. Examine the door, hinges, and door actuating 32-00-00-05

linkage for wear, condition, and security.

2. Jack aircraft per the applicable Beechcraft King Air Beechcraft

Maintenance Manual and perform a landing gear King Air MM
retraction test.

3. Examine the door retraction linkage for proper 32-00-00-20

operation and adjustment.

4. Examine the doors for proper fit and security when 32-00-00-20
the landing gear is retracted.

5. Perform a Manual/Emergency landing gear Beechcraft

extension test per the applicable Beechcraft King Air King Air MM
Maintenance Manual.

E. WING LOCKERS LH 50-00-00-00 -- --

1. Examine Locker Shell for condition and security. 50-00-00-05

2. Examine Locker Door for condition and security. 50-00-00-05

3. Examine Latches for condition and security. 50-00-00-05

4. Examine Hinges for condition and security. 50-00-00-05

5. Examine the Flap Fairing for condition and security 50-00-00-05

of attachment.

Revision AM 37
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-04 Phase 4 or Detailed 4 Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

F. WING LOCKER RH 50-00-00-00 -- --

1. Examine Locker Shell for condition and security. 50-00-00-05

2. Examine Locker Door for condition and security. 50-00-00-05

3. Examine Latches for condition and security. 50-00-00-05

4. Examine Hinges for condition and security. 50-00-00-05

5. Inspect the Flap Fairing for condition and security of 50-00-00-05

attachment.

G. DUAL AFT BODY STRAKES LH 53-00-00-00 -- --

1. Examine Strake for condition and security. 53-00-00-05

2. Examine drain holes for obstructions. 53-00-00-05

H. DUAL AFT BODY STRAKES RH 53-00-00-00 -- --

1. Examine Strake for condition and security. 53-00-00-05

2. Examine drain holes for obstructions. 53-00-00-05

I. EXHAUST FAIRINGS LH 54-00-00-00 -- --

1. Examine Fairings for condition and security. 54-00-00-05

2. Examine fasteners for condition and security. 54-00-00-05

3. Remove Fairings and examine gasket for condition. 54-00-00-05

Revision AM 38
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-04 Phase 4 or Detailed 4 Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

J. EXHAUST FAIRINGS RH 54-00-00-00 -- --

1. Examine Fairings for condition and security. 54-00-00-05

2. Examine fasteners for condition and security. 54-00-00-05

3. Remove Fairings and examine gasket for condition. 54-00-00-05

K. ENHANCED PERFORMANCE LEADING EDGE LH 57-00-00-00 -- --

1. Examine the de-ice boot for condition and security. 30-57-00-05

2. Examine the intercooler duct and gasket for 57-00-00-05

condition and security.

3. Examine the Wing-to-Body Fairing for condition and 57-00-00-05

security.

4. Using Non-destructive Testing (NDT), such as a 57-00-00-05

manual tap test, examine the leading edge for
delamination.

L. ENHANCED PERFORMANCE LEADING EDGE RH 57-00-00-00 -- --

1. Examine the de-ice boot for condition and security. 30-57-00-05

2. Examine the intercooler duct and gasket for 57-00-00-05

condition and security.

3. Examine the Wing-to-Body Fairing for condition and 57-00-00-05

security.

4. Using Non-destructive Testing (NDT), such as a 57-00-00-05

manual tap test, examine the leading edge for
delamination.

Revision AM 39
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-04 Phase 4 or Detailed 4 Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

PROPELLERS
*Use appropriate Subject for your airplane Model and
blade design. SYSTEM

61-00-XX*-00

Subject 10 90 Series Quiet Turbofan Propellers

Subject 11 90 Series Swept Turbofan Propellers

Subject 20 F90 Quiet Turbofan Propellers

Subject 30 100 Series Quiet Turbofan Propellers

Subject 40 200 Series Quiet Turbofan Propellers

Subject 41 200 Series Swept Turbofan Propellers

200 Series Five-Blade Swept Turbofan

Subject 42
Propellers

Subject 51 300/300LW, B300/B300C Four-Blade Swept

Turbofan Propellers

Subject 52 300/300LW, B300/B300 Five-Blade Swept

Turbofan Propellers

M. PROPELLERS LH 61-00-XX*-00 -- --

1. Inspect propeller de-ice system for condition and 30-61-00-05

security (spinner removal required).

2. Inspect Propeller for condition and security. 61-00-XX*-05

N. PROPELLERS RH 61-00-XX*-00 -- --

1. Inspect Propeller de-ice system for condition and 30-61-00-05

security (spinner removal required).

2. Inspect Propeller for condition and security. 61-00-XX*-05

Revision AM 40
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-04 Phase 4 or Detailed 4 Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

O. ENGINE TRUSS LH 71-00-00-00

200 SERIES, 300/300LW, B300/B300C -- --
EQUIPPED WITH FIVE-BLADE SWEPT
TURBOFAN PROPELLERS

1. Inspect for cracks, dents, chafing, and corrosion. 71-00-00-05

Special attention should be made to areas around
clamps.

2. Inspect vibration isolators (mounts) for deterioration, 71-00-00-05

damage, and attachment.

P. ENGINE TRUSS RH 71-00-00-00

200 SERIES, 300/300LW, B300/B300C -- --
EQUIPPED WITH FIVE-BLADE SWEPT
TURBOFAN PROPELLERS

1. Inspect for cracks, dents, chafing, and corrosion. 71-00-00-05

Special attention should be made to areas around -- --
clamps.

2. Inspect vibration isolators (mounts) for deterioration, 71-00-00-05

damage, and attachment.

Q. FUNCTIONAL CHECKS Beechcraft

-- --
King Air MM

1. Perform all Operational Inspection items per the Beechcraft

applicable Beechcraft King Air Maintenance Manual, King Air MM
Scheduled Inspection Program (Phase/Detailed 2 &
4).

R. POST INSPECTION ITEMS -- -- --

1. Lubricate as necessary 12-00-00-00

2. Determine that all required placards are in place and 11-00-00-00

legible.

3. Complete all necessary logbook entries. --

Revision AM 41
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-04 Phase 4 or Detailed 4 Inspection Discrepancy Sheet

05-20-00-04 Phase 4 or Detailed 4 Inspection Discrepancy Sheet

DISCREPANCY CORRECTIVE ACTION MECH INSP

Revision AM 42
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-05 HUIP Routine Inspection

05-20-00-05 HUIP Routine Inspection

ATA
SYSTEM MECH INSP
REFERENCE

A. RAM AIR RECOVERY SYSTEM LH 30-00-00-00 -- --

1. Examine Diaphragm Seals for condition and 30-70-00-05

security.

2. Examine Bypass Door Seals for condition and 30-72-00-05

security.

3. Examine Particle Separator for condition and 30-72-00-05

security.

4. Examine Fixed Turning Vane for condition and 30-72-00-05

security.

5. Examine Ice Shedder Screen for condition and 30-72-00-05

security.

B. RAM AIR RECOVERY SYSTEM RH 30-00-00-00 -- --

1. Examine Diaphragm Seals for condition and 30-70-00-05

security.

2. Examine Bypass Door Seals for condition and 30-72-00-05

security.

3. Examine Particle Separator for condition and 30-72-00-05

security.

4. Examine Fixed Turning Vane for condition and 30-72-00-05

security.

5. Examine Ice Shedder Screen for condition and 30-72-00-05

security.

C. FULLY ENCLOSED MLG DOORS LH 32-00-00-00 -- --

1. Examine door hinges and door actuating linkage for 32-00-00-05

security and condition.

D. FULLY ENCLOSED MLG DOORS RH 32-00-00-00 -- --

1. Examine door hinges and door actuating linkage for 32-00-00-05

security and condition.

Revision AM 43
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-05 HUIP Routine Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

E. WING LOCKERS LH 50-00-00-00 -- --

1. Examine Locker Shell for condition and security. 50-00-00-05

2. Examine Locker Door for condition and security. 50-00-00-05

3. Examine Latches for condition and security. 50-00-00-05

4. Examine Hinges for condition and security. 50-00-00-05

5. Examine the Flap Fairing for condition and security 50-00-00-05

of attachment.

F. WING LOCKERS RH 50-00-00-00 -- --

1. Examine Locker Shell for condition and security. 50-00-00-05

2. Examine Locker Door for condition and security. 50-00-00-05

3. Examine Latches for condition and security. 50-00-00-05

4. Examine Hinges for condition and security. 50-00-00-05

5. Examine the Flap Fairing for condition and security 50-00-00-05

of attachment.

G. DUAL AFT BODY STRAKES LH 53-00-00-00 -- --

1. Examine Strake for condition and security. 53-00-00-05

2. Examine drain holes for obstructions. 53-00-00-05

H. DUAL AFT BODY STRAKES RH 53-00-00-00 -- --

1. Examine Strake for condition and security. 53-00-00-05

2. Examine drain holes for obstructions. 53-00-00-05

I. EXHAUST FAIRINGS LH 54-00-00-00 -- --

1. Examine Fairings for condition and security. 54-00-00-05

J. EXHAUST FAIRINGS RH 54-00-00-00 -- --

1. Examine Fairings for condition and security 54-00-00-05

Revision AM 44
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-05 HUIP Routine Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

K. ENHANCED PERFORMANCE LEADING EDGE LH 57-00-00-00 -- --

1. Examine the de-ice boot for condition and security. 30-57-00-05

2. Using Non-destructive Testing (NDT), such as a 57-00-00-05

manual tap test, examine exterior surface for
delaminations.

3. If exterior delamination detected, use NDT to 57-00-00-05

examine interior surface of cored areas.

L. ENHANCED PERFORMANCE LEADING EDGE RH 57-00-00-00 -- --

1. Examine the de-ice boot for condition and security. 30-57-00-05

2. Using Non-destructive Testing (NDT), such as a 57-00-00-05

manual tap test, examine exterior surface for
delaminations.

3. If exterior delamination detected, use NDT to 57-00-00-05

examine interior surface of cored areas.

PROPELLERS
*Use appropriate Subject for your airplane Model and
blade design. SYSTEM

61-00-XX*-00

Subject 40 200 Series Quiet Turbofan Propellers

Subject 41 200 Series Swept Turbofan Propellers

Subject 42 200 Series Five-Blade Swept Turbofan

Propellers

Subject 51 B300/B300C Four-Blade Swept Turbofan

Propellers

Subject 52 B300/B300C Five-Blade Swept Turbofan

Propellers

M. PROPELLERS LH 61-00-XX*-00 -- --

1. Inspect propeller de-ice boots for condition and 30-61-XX*-05

security.

2. Remove spinner and inspect de-ice boot wiring for 61-00-XX*-05

condition and security.

Revision AM 45
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-05 HUIP Routine Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

N. PROPELLERS RH 61-00-XX*-00 -- --

1. Inspect propeller de-ice boots for condition and 30-61-XX*-05

security.

2. Remove spinner and inspect de-ice boot wiring for 61-00-XX*-05

condition and security.

O. ENGINE TRUSS LH 71-00-00-00

200 SERIES, B300/B300C -- --
EQUIPPED WITH FIVE-BLADE SWEPT
TURBOFAN PROPELLERS

1. Inspect for cracks, dents, chafing, and corrosion. 71-00-00-05

Special attention should be made to areas around
clamps.

2. Inspect vibration isolators (mounts) for deterioration, 71-00-00-05

damage, and attachment.

P. ENGINE TRUSS RH 71-00-00-00

200 SERIES, B300/B300C -- --
EQUIPPED WITH FIVE-BLADE SWEPT
TURBOFAN PROPELLERS

1. Inspect for cracks, dents, chafing, and corrosion. 71-00-00-05

Special attention should be made to areas around -- --
clamps.

2. Inspect vibration isolators (mounts) for deterioration, 71-00-00-05

damage, and attachment.

Q. POST INSPECTION ITEMS -- -- --

1. Lubricate as necessary. 12-00-00-00

2. Determine that all required placards are in place and 11-00-00-00

legible.

3. Complete all necessary logbook entries. --

R. FUNCTIONAL CHECKS Beechcraft

-- --
King Air MM

1. Perform all Operational Inspection items per the Beechcraft

applicable Beechcraft King Air Maintenance Manual, King Air MM
HUIP Inspection Program Routine Inspection

Revision AM 46
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-05 HUIP Routine Inspection Discrepancy Sheet

05-20-00-05 HUIP Routine Inspection Discrepancy Sheet

DISCREPANCY CORRECTIVE ACTION MECH INSP

Revision AM 47
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-06 HUIP Inspection: Detailed 1, 2, 3, & 4

05-20-00-06 HUIP Inspection: Detailed 1, 2, 3, & 4

ATA
SYSTEM MECH INSP
REFERENCE

A. RAM AIR RECOVERY SYSTEM LH 30-00-00-00 -- --

1. Examine the Aft Bulkhead Seals for condition, 30-72-00-05

attachment, and sealing conditions.

2. Examine the Bypass Door Seals for condition, 30-72-00-05

attachment, and sealing conditions. Examine for
freedom of movement and correct adjustment.

3. Examine the Particle Separator for structural 30-72-00-05

condition and attachment. Examine for freedom of
movement and proper travel.

4. Examine the Fixed Turning Vane for structural 30-72-00-05

condition and attachment.

5. Examine the Ice Shedder Screen for condition and 30-72-00-05

attachment.

B. RAM AIR RECOVERY SYSTEM RH 30-00-00-00 -- --

1. Examine the Aft Bulkhead Seals for condition, 30-72-00-05

attachment, and sealing conditions.

2. Examine the Bypass Door Seals for condition, 30-72-00-05

attachment, and sealing conditions. Examine for
freedom of movement and correct adjustment.

3. Examine the Particle Separator for structural 30-72-00-05

condition and attachment. Examine for freedom of
movement and proper travel.

4. Examine the Fixed Turning Vane for structural 30-72-00-05

condition and attachment.

5. Examine the Ice Shedder Screen for condition and 30-72-00-05

attachment.

Revision AM 48
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-06 HUIP Inspection: Detailed 1, 2, 3, & 4 (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

C. FULLY ENCLOSED MLG DOORS LH 32-00-00-00 -- --

1. Examine the door, hinges, and door actuating 32-00-00-05

linkage for wear, condition, and security.

2. Detailed Inspection 4 only: Beechcraft

Jack aircraft per the applicable Beechcraft King Air King Air MM
Maintenance Manual and perform a landing gear
retraction test.

3. Examine the door retraction linkage for proper 32-00-00-20

operation and adjustment.

4. Examine the doors for proper fit and security when 32-00-00-20
the landing gear is retracted.

5. Perform a Manual/Emergency landing gear Beechcraft

extension test per the applicable Beechcraft King Air King Air MM
Maintenance Manual.

D. FULLY ENCLOSED MLG DOORS RH 32-00-00-00 -- --

1. Examine the door, hinges, and door actuating 32-00-00-05

linkage for wear, condition, and security.

2. Detailed Inspection 4 only: Beechcraft

Jack aircraft per the applicable Beechcraft King Air King Air MM
Maintenance Manual and perform a landing gear
retraction test.

3. Examine the door retraction linkage for proper 32-00-00-20

operation and adjustment.

4. Examine the doors for proper fit and security when 32-00-00-20
the landing gear is retracted.

5. Perform a Manual/Emergency landing gear Beechcraft

extension test per the applicable Beechcraft King Air King Air MM
Maintenance Manual.

E. WING LOCKERS LH 50-00-00-00 -- --

1. Examine Locker Shell for condition and security. 50-00-00-05

2. Examine Locker Door for condition and security. 50-00-00-05

3. Examine Latches for condition and security. 50-00-00-05

4. Examine Hinges for condition and security. 50-00-00-05

5. Examine the Flap Fairing for condition and security 50-00-00-05

of attachment.

Revision AM 49
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-06 HUIP Inspection: Detailed 1, 2, 3, & 4 (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

F. WING LOCKER RH 50-00-00-00 -- --

1. Examine Locker Shell for condition and security. 50-00-00-05

2. Examine Locker Door for condition and security. 50-00-00-05

3. Examine Latches for condition and security. 50-00-00-05

4. Examine Hinges for condition and security. 50-00-00-05

5. Inspect the Flap Fairing for condition and security of 50-00-00-05

attachment.

G. DUAL AFT BODY STRAKES LH 53-00-00-00 -- --

1. Examine Strake for condition and security. 53-00-00-05

2. Examine drain holes for obstructions. 53-00-00-05

H. DUAL AFT BODY STRAKES RH 53-00-00-00 -- --

1. Examine Strake for condition and security. 53-00-00-05

2. Examine drain holes for obstructions. 53-00-00-05

I. EXHAUST FAIRINGS LH 54-00-00-00 -- --

1. Examine Fairings for condition and security. 54-00-00-05

2. Examine fasteners for condition and security. 54-00-00-05

3. Remove Fairings and examine gasket for condition. 54-00-00-05

J. EXHAUST FAIRINGS RH 54-00-00-00 -- --

1. Examine Fairings for condition and security. 54-00-00-05

2. Examine fasteners for condition and security. 54-00-00-05

3. Remove Fairings and examine gasket for condition. 54-00-00-05

Revision AM 50
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-06 HUIP Inspection: Detailed 1, 2, 3, & 4 (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

K. ENHANCED PERFORMANCE LEADING EDGE LH 57-00-00-00 -- --

1. Examine the de-ice boot for condition and security. 30-57-00-05

2. Examine the intercooler duct and gasket for 57-00-00-05

condition and security.

3. Examine the Wing-to-Body Fairing for condition and 57-00-00-05

security.

4. Using Non-destructive Testing (NDT), such as a 57-00-00-05

manual tap test, examine the leading edge for
delamination. Examine both sides of core.

5. Remove the Wing-to-Body Fairing. Inspect the 57-00-00-05

fairing, leading edge, and fuselage for condition and
chafing.

6. Remove the inboard Leading Edge. Inspect the 57-00-00-05

inner surface of the leading edge for condition and
delamination. Inspect the intercooler duct for
condition.

L. ENHANCED PERFORMANCE LEADING EDGE RH 57-00-00-00 -- --

1. Examine the de-ice boot for condition and security. 30-57-00-05

2. Examine the intercooler duct and gasket for 57-00-00-05

condition and security.

3. Examine the Wing-to-Body Fairing for condition and 57-00-00-05

security.

4. Using Non-destructive Testing (NDT), such as a 57-00-00-05

manual tap test, examine the leading edge for
delamination. Examine both sides of core.

5. Remove the Wing-to-Body Fairing. Inspect the 57-00-00-05

fairing, leading edge, and fuselage for condition and
chafing.

6. Remove the inboard Leading Edge. Inspect the 57-00-00-05

inner surface of the leading edge for condition and
delamination. Inspect the intercooler duct for
condition.

Revision AM 51
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-06 HUIP Inspection: Detailed 1, 2, 3, & 4 (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

PROPELLERS
*Use appropriate Subject for your airplane Model and
blade design. SYSTEM

61-00-XX*-00

Subject 40 200 Series Quiet Turbofan Propellers

Subject 41 200 Series Swept Turbofan Propellers

200 Series Five-Blade Swept Turbofan

Subject 42
Propellers

B300/B300C Four-Blade Swept Turbofan

Subject 51
Propellers

B300/B300C Five-Blade Swept Turbofan

Subject 52
Propellers

M. PROPELLERS LH 61-00-XX*-00 -- --

1. Inspect propeller de-ice system for condition and 30-61-00-05

security (spinner removal required).

2. Inspect Propeller for condition and security. 61-00-XX*-05

N. PROPELLERS RH 61-00-XX*-00 -- --

1. Inspect Propeller de-ice system for condition and 30-61-00-05

security (spinner removal required).

2. Inspect Propeller for condition and security. 61-00-XX*-05

Revision AM 52
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-06 HUIP Inspection: Detailed 1, 2, 3, & 4 (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

O. ENGINE TRUSS LH 71-00-00-00

200 SERIES, B300/B300C -- --
EQUIPPED WITH FIVE-BLADE SWEPT
TURBOFAN PROPELLERS

1. Inspect for cracks, dents, chafing, and corrosion. 71-00-00-05

Special attention should be made to areas around
clamps.

2. Inspect vibration isolators (mounts) for deterioration, 71-00-00-05

damage, and attachment.

P. ENGINE TRUSS RH 71-00-00-00

200 SERIES, B300/B300C -- --
EQUIPPED WITH FIVE-BLADE SWEPT
TURBOFAN PROPELLERS

1. Inspect for cracks, dents, chafing, and corrosion. 71-00-00-05

Special attention should be made to areas around
clamps.

2. Inspect vibration isolators (mounts) for deterioration, 71-00-00-05

damage, and attachment.

Q. POST INSPECTION ITEMS -- -- --

1. Lubricate as necessary. 12-00-00-00

2. Determine that all required placards are in place and 11-00-00-00

legible.

3. Complete all necessary logbook entries. --

R. FUNCTIONAL CHECKS Beechcraft

-- --
King Air MM

1. Perform all Operational Inspection items per the Beechcraft

applicable Beechcraft King Air Maintenance Manual, King Air MM
HUIP Inspection Program (Detail 1, 2, 3, or 4).

Revision AM 53
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-06 HUIP Inspection: Detailed 1, 2, 3, & 4 Discrepancy Sheet

05-20-00-06 HUIP Inspection: Detailed 1, 2, 3 & 4 Discrepancy Sheet

DISCREPANCY CORRECTIVE ACTION MECH INSP

Revision AM 54
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-07 Alternate Phase Inspection

Reference 05-20-00-01, 05-20-00-02, 05-20-00-03, and 05-20-00-04 Phase Inspections for Alternate
Phase Inspections and Discrepancy Sheets.

05-20-00-08 Biennial: Interim Inspection

05-20-00-08 Biennial: Interim Inspection

ATA
SYSTEM MECH INSP
REFERENCE

A. RAM AIR RECOVERY SYSTEM LH 30-00-00-00 -- --

1. Inspect engine inertial anti-icer for proper operation 30-72-00-05

and rigging.

B. RAM AIR RECOVERY SYSTEM RH 30-00-00-00 -- --

1. Inspect engine inertial anti-icer for proper operation 30-72-00-05

and rigging.

C. FULLY ENCLOSED MLG DOORS LH 32-00-00-00 -- --

1. Examine the door, hinges, and door actuating 32-00-00-05

linkage for condition, and security.

D. FULLY ENCLOSED MLG DOORS RH 32-00-00-00 -- --

1. Examine the door, hinges, and door actuating 32-00-00-05

linkage for condition, and security.

E. WING LOCKERS LH 50-00-00-00 -- --

1. Examine Lockers, Doors, Latches, Hinges, and Flap 50-00-00-05

Fairing for condition and security.

F. WING LOCKER RH 50-00-00-00 -- --

1. Examine Lockers, Doors, Latches, Hinges and Flap 50-00-00-05

Fairing for condition and security.

G. DUAL AFT BODY STRAKES LH 53-00-00-00 -- --

1. Examine Strake for condition and security. 53-00-00-05

2. Examine drain holes for obstructions. 53-00-00-05

H. DUAL AFT BODY STRAKES RH 53-00-00-00 -- --

1. Examine Strake for condition and security. 53-00-00-05

2. Examine drain holes for obstructions. 53-00-00-05

Revision AM 55
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-08 Biennial: Interim Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

I. EXHAUST FAIRINGS LH 54-00-00-00 -- --

1. Examine Fairings for condition and security. 54-00-00-05

J. EXHAUST FAIRINGS RH 54-00-00-00 -- --

1. Examine Fairings for condition and security. 54-00-00-05

K. ENHANCED PERFORMANCE LEADING EDGE LH 57-00-00-00 -- --

1. Check surface de-ice system for proper operation 30-57-00-05

and cycling.

L. ENHANCED PERFORMANCE LEADING EDGE RH 57-00-00-00 -- --

1. Check surface de-ice system for proper operation 30-57-00-05

and cycling.

Revision AM 56
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-08 Biennial: Interim Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

PROPELLERS
*Use appropriate Subject for your airplane Model and
blade design. SYSTEM

61-00-XX*-00

Subject 10 90 Series Quiet Turbofan Propellers

Subject 11 90 Series Swept Turbofan Propellers

Subject 20 F90 Quiet Turbofan Propellers

Subject 30 100 Series Quiet Turbofan Propellers

Subject 40 200 Series Quiet Turbofan Propellers

Subject 41 200 Series Swept Turbofan Propellers

Subject 42 200 Series Five-Blade Swept Turbofan

Propellers

Subject 51 300/300LW, B300/B300C Four-Blade Swept

Turbofan Propellers

Subject 52 300/300LW, B300/B300C Five-Blade Swept

Turbofan Propellers

M. PROPELLERS LH 61-00-XX*-00 -- --

1. Check de-ice boots for proper operation and cycling. 30-61-00-05

2. Perform flight idle torque check. 61-00-XX*-05

N. PROPELLERS RH 61-00-XX*-00 -- --

1. Check de-ice boots for proper operation and cycling. 30-61-00-05

2. Perform flight idle torque check. 61-00-XX*-05

Revision AM 57
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-08 Biennial: Interim Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

O. ENGINE TRUSS LH 71-00-00-00 -- --

200 SERIES, 300/300LW, B300/B300C
EQUIPPED WITH FIVE-BLADE SWEPT
TURBOFAN PROPELLERS

1. Inspect for cracks, dents, chafing, and corrosion. 71-00-00-05

Special attention should be made to areas around
clamps.

2. Inspect vibration isolators (mounts) for deterioration, 71-00-00-05

damage, and attachment.

P. ENGINE TRUSS RH 71-00-00-00 -- --

200 SERIES, 300/300LW, B300/B300C
EQUIPPED WITH FIVE-BLADE SWEPT
TURBOFAN PROPELLERS

1. Inspect for cracks, dents, chafing, and corrosion. 71-00-00-05

Special attention should be made to areas around
clamps.

2. Inspect vibration isolators (mounts) for deterioration, 71-00-00-05

damage, and attachment.

Q. FUNCTIONAL CHECKS Beechcraft -- --

King Air MM

1. Perform all Operational Inspection items per the Beechcraft

applicable Beechcraft King Air Maintenance Manual, King Air MM
Scheduled Inspection Program.

R. POST INSPECTION ITEMS -- -- --

1. Lubricate as necessary. 12-00-00-00

2. Determine that all required placards are in place and 11-00-00-00

legible.

3. Complete all necessary logbook entries. --

Revision AM 58
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-08 Biennial: Interim Inspection Discrepancy Sheet

05-20-00-08 Biennial: Interim Inspection Discrepancy Sheet

DISCREPANCY CORRECTIVE ACTION MECH INSP

Revision AM 59
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-09 Biennial: Complete Inspection

05-20-00-09 Biennial: Complete Inspection

ATA
SYSTEM MECH INSP
REFERENCE

A. RAM AIR RECOVERY SYSTEM LH 30-00-00-00 -- --

1. Examine the Diaphragm Seals for condition, 30-72-00-05

attachment, and sealing conditions.

2. Examine the Bypass Door Seals for condition, 30-72-00-05

attachment, and sealing conditions. Examine for
freedom of movement and correct adjustment.

3. Examine the Particle Separator for structural 30-72-00-05

condition and attachment. Examine for freedom of
movement and proper travel.

4. Examine the Fixed Turning Vane for structural 30-72-00-05

condition and attachment.

5. Examine the Ice Shedder Screen for condition and 30-72-00-05

attachment.

B. RAM AIR RECOVERY SYSTEM RH 30-00-00-00 -- --

1. Examine the Diaphragm Seals for condition, 30-72-00-05

attachment, and sealing conditions.

2. Examine the Bypass Door Seals for condition, 30-72-00-05

attachment, and sealing conditions. Examine for
freedom of movement and correct adjustment.

3. Examine the Particle Separator for structural 30-72-00-05

condition and attachment. Examine for freedom of
movement and proper travel.

4. Examine the Fixed Turning Vane for structural 30-72-00-05

condition and attachment.

5. Examine the Ice Shedder Screen for condition and 30-72-00-05

attachment.

Revision AM 60
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-09 Biennial: Complete Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

C. FULLY ENCLOSED MLG DOORS LH 32-00-00-00 -- --

1. Examine the door, hinges, and door actuating 32-00-00-05

linkage for wear, condition, and security.

2. Jack Aircraft per the applicable Beechcraft King Air Beechcraft

Maintenance Manual and perform a landing gear King Air MM
retraction test.

3. Examine the door retraction linkage for proper 32-00-00-20

operation and adjustment.

4. Examine the doors for proper fit and security when 32-00-00-20
the landing gear is retracted.

5. Perform a Manual/Emergency landing gear Beechcraft

extension test per the applicable Beechcraft King Air King Air MM
Maintenance Manual.

D. FULLY ENCLOSED MLG DOORS RH 32-00-00-00 -- --

1. Examine the door, hinges, and door actuating 32-00-00-05

linkage for wear, condition, and security.

2. Jack Aircraft per the applicable Beechcraft King Air Beechcraft

Maintenance Manual and perform a landing gear King Air MM
retraction test.

3. Examine the door retraction linkage for proper 32-00-00-20

operation and adjustment.

4. Examine the doors for proper fit and security when 32-00-00-20
the landing gear is retracted.

5. Perform a Manual/Emergency landing gear Beechcraft

extension test per the applicable Beechcraft King Air King Air MM
Maintenance Manual.

E. WING LOCKERS LH 50-00-00-00 -- --

1. Examine Locker Shell for condition and security. 50-00-00-05

2. Examine Locker Door for condition and security. 50-00-00-05

3. Examine Latches for condition and security. 50-00-00-05

4. Examine the Hinges for condition and security. 50-00-00-05

5. Examine Flap Fairing for condition and security of 50-00-00-05

attachment.

Revision AM 61
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-09 Biennial: Complete Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

F. WING LOCKER RH 50-00-00-00 -- --

1. Examine Locker Shell for condition and security. 50-00-00-05

2. Examine Locker Door for condition and security. 50-00-00-05

3. Examine Latches for condition and security. 50-00-00-05

4. Examine the Hinges for condition and security. 50-00-00-05

5. Examine Flap Fairing for condition and security of 50-00-00-05

attachment.

G. DUAL AFT BODY STRAKES LH 53-00-00-00 -- --

1. Examine Strake for condition and security. 53-00-00-05

2. Examine drain holes for obstructions. 53-00-00-05

H. DUAL AFT BODY STRAKES RH 53-00-00-00 -- --

1. Examine Strake for condition and security. 53-00-00-05

2. Examine drain holes for obstructions. 53-00-00-05

I. EXHAUST FAIRINGS LH 54-00-00-00 -- --

1. Examine Fairings for condition and security. 54-00-00-05

2. Examine fasteners for condition and security. 53-00-00-05

3. Remove Fairings and examine gasket for condition. 53-00-00-05

J. EXHAUST FAIRINGS RH 54-00-00-00 -- --

1. Examine Fairings for condition and security. 54-00-00-05

2. Examine fasteners for condition and security. 54-00-00-05

3. Remove Fairings and examine gasket for condition. 54-00-00-05

Revision AM 62
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-09 Biennial: Complete Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

K. ENHANCED PERFORMANCE LEADING EDGE LH 57-00-00-00 -- --

1. Examine the de-ice boot for condition and security. 30-57-00-05

2. Check surface de-ice system for proper operation 30-57-00-05

and cycling.

3. Examine the intercooler duct and gasket for 57-00-00-05

condition and security.

4. Examine the Wing-to-Body fairing for condition and 57-00-00-05

security.

5. Using Non-destructive Testing (NDT), such as a 57-00-00-05

manual tap test, examine the leading edge for
delamination. Examine both sides of core.

6. Remove the Wing-to-Body Fairing. Inspect the 57-00-00-05

fairing, leading edge, and fuselage for condition and
chafing.

7. Remove the inboard Leading Edge. Inspect the 57-00-00-05

inner surface of the leading edge for condition and
delamination. Inspect the intercooler duct for
condition.

L. ENHANCED PERFORMANCE LEADING EDGE RH 57-00-00-00 -- --

1. Examine the de-ice boot for condition and security. 30-57-00-05

2. Check surface de-ice system for proper operation 30-57-00-05

and cycling.

3. Examine the intercooler duct and gasket for 57-00-00-05

condition and security.

4. Examine the Wing-to-Body Fairing for condition and 57-00-00-05

security.

5. Using Non-destructive Testing (NDT), such as a 57-00-00-05

manual tap test, examine the leading edge for
delamination. Examine both sides of core.

6. Remove the Wing-to-Body Fairing. Inspect the 57-00-00-05

fairing, leading edge, and fuselage for condition and
chafing.

7. Remove the inboard Leading Edge. Inspect the 57-00-00-05

inner surface of the leading edge for condition and
delamination. Inspect the intercooler duct for
condition.

Revision AM 63
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-09 Biennial: Complete Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

M. OUTBOARD WING LH 57-00-00-00 -- --

C90A AND C90GT ONLY LJ-1138 THRU
LJ-1145 AND LJ-1147 AND AFTER WITH
OPTIONAL GROSS WEIGHT INCREASE

1. Remove the lower Wing Tip Attachment Cover, 57-57-00-05

Panel 20. Inspect the Ballast Weight and Wing Tip 57-61-10-05
Center Rib (000-170012-3) for condition and 57-61-11-05
security.
CAUTION: THE RETAINING HARDWARE IS NON-
MAGNETIC. USE OF MAGNETIC
HARDWARE CAN INTERFERE WITH
THE AIRCRAFT’S NAVIGATION
SYSTEM. IF THE BALLAST WEIGHT IS
REMOVED ENSURE IT IS REINSTALLED
USING THE CORRECT HARDWARE.

2. Re-install the Access Panel, verifying use of correct Beechcraft

hardware. King Air MM

N. OUTBOARD WING RH 57-00-00-00 -- --

C90A AND C90GT ONLY LJ-1138 THRU
LJ-1145 AND LJ-1147 AND AFTER WITH
OPTIONAL GROSS WEIGHT INCREASE

1. Remove the lower Wing Tip Attachment Cover, 57-57-00-05

Panel 20. Inspect the Ballast Weight and Wing Tip 57-61-10-05
Center Rib (000-170012-4) for condition and 57-61-11-05
security.
CAUTION: THE RETAINING HARDWARE IS NON-
MAGNETIC. USE OF MAGNETIC
HARDWARE CAN INTERFERE WITH
THE AIRCRAFT’S NAVIGATION
SYSTEM. IF THE BALLAST WEIGHT IS
REMOVED ENSURE IT IS REINSTALLED
USING THE CORRECT HARDWARE.

2. Re-install the Access Panel, verifying use of correct Beechcraft

hardware. King Air MM

Revision AM 64
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-09 Biennial: Complete Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

O. OUTBOARD WING LH 57-00-00-00 -- --

100 SERIES ONLY, B-2 THRU B-89 & B93 WITH
GROSS WEIGHT INCREASE

1. Inspect the Ballast Weight for condition and security 57-61-30-05

of attachment.
CAUTION: THE RETAINING HARDWARE IS NON-
MAGNETIC. USE OF MAGNETIC
HARDWARE CAN INTERFERE WITH
THE AIRCRAFT’S NAVIGATION
SYSTEM. IF THE BALLAST WEIGHT IS
REMOVED ENSURE IT IS REINSTALLED
USING THE CORRECT HARDWARE.

P. OUTBOARD WING RH 57-00-00-00 -- --

100 SERIES ONLY, B-2 THRU B-89 & B93 WITH
GROSS WEIGHT INCREASE

1. Inspect the Ballast Weight for condition and security 57-61-30-05

of attachment.
CAUTION: THE RETAINING HARDWARE IS NON-
MAGNETIC. USE OF MAGNETIC
HARDWARE CAN INTERFERE WITH
THE AIRCRAFT’S NAVIGATION
SYSTEM. IF THE BALLAST WEIGHT IS
REMOVED ENSURE IT IS REINSTALLED
USING THE CORRECT HARDWARE.

2. Examine Flap Fairing for condition and security of 50-00-00-05

attachment.

Revision AM 65
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-09 Biennial: Complete Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

PROPELLERS
*Use appropriate Subject for your airplane Model and
blade design. SYSTEM

61-00-XX*-00

Subject 10 90 Series Quiet Turbofan Propellers

Subject 11 90 Series Swept Turbofan Propellers

Subject 20 F90 Quiet Turbofan Propellers

Subject 30 100 Series Quiet Turbofan Propellers

Subject 40 200 Series Quiet Turbofan Propellers

Subject 41 200 Series Swept Turbofan Propellers

Subject 42 200 Series Five-Blade Swept Turbofan

Propellers

Subject 51 300/300LW, B300/B300C Four-Blade Swept

Turbofan Propellers

Subject 52 300/300LW, B300/B300C Five-Blade Swept

Turbofan Propellers

Q. PROPELLERS LH 61-00-XX*-00 -- --

1. Inspect propeller de-ice system for condition and 30-61-00-05

security (spinner removal required).

2. Check de-ice boots for proper operation and cycling. 30-61-00-05

3. Inspect Propeller for condition and security. 61-00-XX*-05

4. Perform flight idle torque check. 61-00-XX*-05

R. PROPELLERS RH 61-00-XX*-00 -- --

1. Inspect propeller de-ice system for condition and 30-61-00-05

security (spinner removal required).

2. Check de-ice boots for proper operation and cycling. 30-61-00-05

3. Inspect Propeller for condition and security. 61-00-XX*-05

4. Perform flight idle torque check. 61-00-XX*-05

Revision AM 66
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-09 Biennial: Complete Inspection (Continued)

ATA
SYSTEM MECH INSP
REFERENCE

S. ENGINE TRUSS LH 71-00-00-00 -- --

200 SERIES, 300/300LW, B300/B300C
EQUIPPED WITH FIVE-BLADE SWEPT
TURBOFAN PROPELLERS

1. Inspect for cracks, dents, chafing, and corrosion. 71-00-00-05

Special attention should be made to areas around
clamps.

2. Inspect vibration isolators (mounts) for deterioration, 71-00-00-05

damage, and attachment.

T. ENGINE TRUSS RH 71-00-00-00 -- --

200 SERIES, 300/300LW, B300/B300C
EQUIPPED WITH FIVE-BLADE SWEPT
TURBOFAN PROPELLERS

1. Inspect for cracks, dents, chafing, and corrosion. 71-00-00-05

Special attention should be made to areas around
clamps.

2. Inspect vibration isolators (mounts) for deterioration, 71-00-00-05

damage, and attachment.

U. FUNCTIONAL CHECKS Beechcraft -- --

King Air MM

1. Perform all Operational Inspection items per the Beechcraft

applicable Beechcraft King Air Maintenance Manual, King Air MM
Scheduled Inspection Program (Phase/Detailed1 &
3).

V. POST INSPECTION ITEMS -- -- --

1. Lubricate as necessary. 12-00-00-00

2. Determine that all required placards are in place and 11-00-00-00

legible.

3. Complete all necessary logbook entries. --

Revision AM 67
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-20-00-09 Biennial: Complete Inspection Discrepancy Sheet

05-20-00-09 Biennial: Complete Inspection Discrepancy Sheet

DISCREPANCY CORRECTIVE ACTION MECH INSP

Revision AM 68
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-21-00-00 Special Inspection Maintenance Practices

The following subchapters are arranged as unscheduled maintenance inspection check lists. When
unscheduled maintenance and detailed secondary inspections are necessary due to operations in
conditions which could require unscheduled maintenance, the affected Raisbeck Airframe,
Powerplant, and Accessory Systems shall be inspected in conjunction with the inspection
requirements set forth in the applicable Beechcraft King Air Maintenance Manual for unscheduled
maintenance.
To facilitate scheduling Special Inspections, Raisbeck Engineering authorizes the inspection interval
tolerances to coincide with the owner’s/operator’s approved maintenance program.

NOTE: Tolerances specified by suppliers, manufactures, DOT regulations, or FAA

regulations take precedence over inspection interval tolerances authorized by
Raisbeck. Tolerances do not accumulate.

Revision AM 69
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-32-00-21 Fully Enclosed MLG Doors Special Inspections

Fully Enclosed MLG Doors Special Inspections

INSPECTION
CONDITION INSPECTION REQUIREMENT
INTERVAL

Operation in Inspect hinges and retraction linkage for condition. Clean Weekly
atmospheres of high salt with low pressure water and mild detergent. Blow dry with
content dry shop air. Lubricate door hinges and retraction linkage
with Dry Film Lubricant, Type A, Class I or II, Grade 1.

Operation in Inspect hinges and retraction linkage for condition. Clean Weekly
atmospheres of high with low pressure water and mild detergent. Blow dry with
industrial air pollution dry shop air. Lubricate door hinges and retraction linkage
with Dry Film Lubricant, Type A, Class I or II, Grade 1.

Operation in areas of If the aircraft is to be operated in areas of high dust Weekly

high dust content content for an extended period of time, thoroughly clean
the door hinges and retraction linkage with cleaning
solvent. Blow dry with dry shop air. Lubricate door hinges
and retraction linkage with Dry Film Lubricant, Type A,
Class I or II, Grade 1.

Operation in areas of Inspect hinges and retraction linkage for condition. Clean Monthly
high humidity with low pressure water and mild detergent. Blow dry with
dry shop air. Lubricate door hinges and retraction linkage
with Dry Film Lubricant, Type A, Class I or II, Grade 1.

Operation from very soft Inspect hinges and retraction linkage for condition. Clean Weekly
or unusual terrain with low pressure water and mild detergent. Blow dry with
dry shop air. Lubricate door hinges and retraction linkage
with Dry Film Lubricant, Type A, Class I or II, Grade 1.

Hard landing Inspect the landing gear in accordance with Chapter 05- As Required
20-02 of this manual, Items C and D.

Encountering turbulent Inspect the landing gear in accordance with Chapter 05- As Required
air 20-02 of this manual, Items C and D.

Inspection after lightning Inspect area of suspected lighting strike for condition. If As Required
strike damage is found, repair or replace affected components.
Inspect the landing gear in accordance with Chapter 05-
20-00-02 of this manual, Items C and D.

Inspection after sudden N/A N/A

stoppage

Inspection after Inspect the landing gear in accordance with Chapter 05- As Required
deploying landing gear 20-02 of this manual, Items C and D.
above critical speed

Inspection after N/A N/A

deploying the flaps
above critical speed

Revision AM 70
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

Fully Enclosed MLG Doors Special Inspections (Continued)

INSPECTION
CONDITION INSPECTION REQUIREMENT
INTERVAL

Operation in or around Inspect hinges and retraction linkage for condition. Clean Weekly
volcanic ash with low pressure water and mild detergent. Blow dry with
dry shop air. Lubricate door hinges and retraction linkage
with Dry Film Lubricant, Type A, Class I or II, Grade 1.

Revision AM 71
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-50-00-21 Wing Lockers Special Inspections

Wing Lockers Special Inspections

INSPECTION
CONDITION INSPECTION REQUIREMENT
INTERVAL

Operation in Inspect hinges and latches for condition. Clean with low Weekly
atmospheres of high salt pressure water and mild detergent. Blow dry with dry
content shop air. Lubricate Hinges with Dry Film Lubricant, Type
A, Class I or II, Grade 1.

Operation in Inspect hinges and latches for condition. Clean with low Weekly
atmospheres of high pressure water and mild detergent. Blow dry with dry
industrial air pollution shop air. Lubricate Hinges with Dry Film Lubricant, Type
A, Class I or II, Grade 1.

Operation in areas of If the aircraft is to be operated in areas of high dust Weekly

high dust content content for an extended period of time, thoroughly clean
the hinges with cleaning solvent. Blow dry with dry shop
air. Lubricate hinges with Dry Film Lubricant, Type A,
Class I or II, Grade 1.

Operation in areas of Inspect hinges and latches for condition. Clean with low Monthly
high humidity pressure water and mild detergent. Blow dry with dry
shop air. Lubricate with Dry Film Lubricant, Type A, Class
I or II, Grade 1.

Operation from very soft Inspect lockers for condition and security. Daily
or unusual terrain

Hard landing Inspect lockers for condition and security. Remove locker As Required
as required to inspect for damage to the airframe.

Encountering turbulent Inspect lockers for condition and security. Remove locker As Required
air as required to inspect for damage to the airframe.

Inspection after lightning Inspect area of suspected lighting strike for condition. If As Required
strike damage is found, repair or replace affected components.

Inspection after sudden N/A N/A

stoppage

Inspection after N/A N/A

deploying landing gear
above critical speed

Inspection after Inspect flap fairings for condition and security. As required
deploying the flaps
above critical speed

Operation in or around Inspect lockers for condition and security. Clean with low Weekly
volcanic ash pressure water and mild detergent. Blow dry with dry
shop air. Lubricate Hinges with Dry Film Lubricant, Type
A, Class I or II, Grade 1.

Revision AM 72
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-51-00-00 Time Limits/Maintenance Checks Airframe Systems

There are no time limited components on any Raisbeck King Air airframe systems. All Raisbeck King
Air airframe components are repaired or replaced when inspection or performance of items reveal a
potentially unsafe condition or performance degradation.

05-61-00-00 Time Limits/Maintenance Checks - Propellers

Time limited components of Raisbeck/Hartzell Swept Turbofan Propeller and Quiet Turbofan
Propeller Systems are defined in Hartzell Propeller Owner’s Manual and Logbook (Manual No. 147,
149, or 486 ATA REF 61-00-47, 61-00-49, or 61-00-86 respectively) and the applicable Beechcraft
King Air Maintenance Manual.
Replacement and overhaul of time limited components of Raisbeck/Hartzell Swept Turbofan Propeller
and Quiet Turbofan Propeller Systems shall be accomplished in accordance with Hartzell Propeller
Owner’s Manual and Logbook (Manual No. 147, 149, or 486 ATA REF 61-00-47, 61-00-49, or 61-00-
86 respectively) and the applicable Beechcraft King Air Maintenance Manual.
Repair or replacement of Raisbeck/Hartzell Swept Turbofan Propeller and Quiet Turbofan Propeller
System assemblies and components not specified in this document shall be accomplished in
accordance with Hartzell Manual No. 147 & 149, ATA REF 61-00-47 & 61-00-49 respectively, and the
applicable Beechcraft King Air Maintenance Manual.

Revision AM 73
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-53-00-21 Dual Aft Body Strakes Special Inspections

Dual Aft Body Strakes Special Inspections

INSPECTION
CONDITION INSPECTION REQUIREMENT
INTERVAL

Operation in Inspect strakes for condition and security. Clean with low Weekly
atmospheres of high salt pressure water and mild detergent.
content

Operation in Inspect strakes for condition and security. Clean with low Weekly
atmospheres of high pressure water and mild detergent.
industrial air pollution

Operation in areas of Inspect strakes for condition and security. Clean with low Weekly
high dust content pressure water and mild detergent.

Operation in areas of Inspect strakes for condition and security. Clean with low Monthly
high humidity pressure water and mild detergent.

Operation from very soft Inspect strakes for condition and security. Daily
or unusual terrain

Hard landing Inspect for condition and security. As required

Encountering turbulent Inspect for condition and security. As required

air

Inspection after lightning Inspect area of suspected lightning strike for condition and As required
strike security. Repair or replace damaged components as
required.

Inspection after sudden N/A N/A

stoppage

Inspection after N/A N/A

deploying landing gear
above critical speed

Inspection after N/A N/A

deploying the flaps
above critical speed

Operation in or around Inspect strakes for condition and security. Clean with low Weekly
volcanic ash pressure water and mild detergent.

Revision AM 74
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-54-00-21 Exhaust Stack Fairings Special Inspections

Exhaust Stack Fairings Special Inspections

INSPECTION
CONDITION INSPECTION REQUIREMENT
INTERVAL

Operation in Inspect fairings for condition and security. Wash with low Weekly
atmospheres of high salt pressure water and mild detergent.
content

Operation in Inspect fairings for condition and security. Wash with low Weekly
atmospheres of high pressure water and mild detergent.
industrial air pollution

Operation in areas of Inspect fairings for condition and security. Wash with low Weekly
high dust content pressure water and mild detergent.

Operation in areas of Inspect fairings for condition and security. Wash with low Weekly
high humidity pressure water and mild detergent.

Operation from very soft Inspect for condition and security. Daily
or unusual terrain

Hard landing Inspect for condition and security. As required

Encountering turbulent Inspect for condition and security. As required

air

Inspection after lightning Inspect area of suspected lightning strike for condition and As required
strike security. Repair or replace damaged components as
required.

Inspection after sudden N/A N/A

stoppage

Inspection after N/A N/A

deploying landing gear
above critical speed

Inspection after N/A N/A

deploying the flaps
above critical speed

Operation in or around Inspect fairings for condition and security. Wash with low Weekly
volcanic ash pressure water and mild detergent.

Revision AM 75
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-57-00-21 Enhanced Performance Leading Edges Special

Inspections
Enhanced Performance Leading Edges Special Inspections

INSPECTION
CONDITION INSPECTION REQUIREMENT
INTERVAL

Operation in Inspect leading edges and de-ice boots for condition and Weekly
atmospheres of high salt security. Wash with low pressure water and mild
content detergent.

Operation in Inspect leading edges and de-ice boots for condition and Weekly
atmospheres of high security. Wash with low pressure water and mild
industrial air pollution detergent.

Operation in areas of Inspect leading edges and de-ice boots for condition and Weekly
high dust content security. Wash with low pressure water and mild
detergent.

Operation in areas of Inspect leading edges and de-ice boots for condition and Monthly
high humidity security. Wash with low pressure water and mild
detergent.

Operation from very soft Inspect for condition and security. Daily
or unusual terrain

Hard landing Inspect for condition and security. Remove leading edges As required
as needed to inspect airframe for damage.

Encountering turbulent Inspect for condition and security. Remove leading edges As required
air as needed to inspect airframe for damage.

Inspection after lightning Inspect area of suspected lightning strike for security and As Required
strike condition. Repair or replace damaged components as
required.

Inspection after sudden N/A N/A

stoppage

Inspection after N/A N/A

deploying landing gear
above critical speed

Inspection after N/A N/A

deploying the flaps
above critical speed

Operation in or around Inspect leading edges and de-ice boots for condition and As Required
volcanic ash security. Wash with low pressure water and mild
detergent.

Revision AM 76
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-61-00-21 Swept Turbofan Propellers, Five-Blade Swept Turbofan

Propellers, and Quiet Turbofan Propellers Special
Inspections
Propellers Special Inspections

CONDITION INSPECTION REQUIREMENT

Operation in The Raisbeck/Hartzell Swept Turbofan Propellers, Five-Blade Swept Turbofan

atmospheres Propellers, and Quiet Turbofan Propellers are to be inspected and maintained in
of high salt accordance with the applicable documents:
content Beechcraft King Air/Super King Air Maintenance Manual
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 147, ATA REF 61-00-47)
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 149, ATA REF 61-00-49)
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 486, ATA REF 61-00-86)
Hartzell Composite Propeller Blade Field Maintenance and Minor Repair Manual
(Manual No. 170, ATA REF 61-13-70)
Hartzell Propeller Ice Protection System Manual (Manual No. 180, ATA REF 30-61-80)

Operation in The Raisbeck/Hartzell Swept Turbofan Propellers, Five-Blade Swept Turbofan

atmospheres Propellers, and Quiet Turbofan Propellers are to be inspected and maintained in
of high accordance with the applicable documents:
industrial air Beechcraft King Air/Super King Air Maintenance Manual
pollution Hartzell Propeller Owner’s Manual and Logbook (Manual No. 147, ATA REF 61-00-47)
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 149, ATA REF 61-00-49)
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 486, ATA REF 61-00-86)
Hartzell Composite Propeller Blade Field Maintenance and Minor Repair Manual
(Manual No. 170, ATA REF 61-13-70)
Hartzell Propeller Ice Protection System Manual (Manual No. 180, ATA REF 30-61-80)

Operation in The Raisbeck/Hartzell Swept Turbofan Propellers, Five-Blade Swept Turbofan

areas of high Propellers, and Quiet Turbofan Propellers are to be inspected and maintained in
dust content accordance with the applicable documents:
Beechcraft King Air/Super King Air Maintenance Manual
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 147, ATA REF 61-00-47)
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 149, ATA REF 61-00-49)
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 486, ATA REF 61-00-86)
Hartzell Composite Propeller Blade Field Maintenance and Minor Repair Manual
(Manual No. 170, ATA REF 61-13-70)
Hartzell Propeller Ice Protection System Manual (Manual No. 180, ATA REF 30-61-80)

Operation in The Raisbeck/Hartzell Swept Turbofan Propellers, Five-Blade Swept Turbofan

areas of high Propellers, and Quiet Turbofan Propellers are to be inspected and maintained in
humidity accordance with the applicable documents:
Beechcraft King Air/Super King Air Maintenance Manual
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 147, ATA REF 61-00-47)
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 149, ATA REF 61-00-49)
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 486, ATA REF 61-00-86)
Hartzell Composite Propeller Blade Field Maintenance and Minor Repair Manual
(Manual No. 170, ATA REF 61-13-70)
Hartzell Propeller Ice Protection System Manual (Manual No. 180, ATA REF 30-61-80)

Revision AM 77
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

Propellers Special Inspections (Continued)

CONDITION INSPECTION REQUIREMENT

Operation from The Raisbeck/Hartzell Swept Turbofan Propellers, Five-Blade Swept Turbofan
very soft or Propellers, and Quiet Turbofan Propellers are to be inspected and maintained in
unusual terrain accordance with the applicable documents:
Beechcraft King Air/Super King Air Maintenance Manual
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 147, ATA REF 61-00-47)
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 149, ATA REF 61-00-49)
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 486, ATA REF 61-00-86)
Hartzell Composite Propeller Blade Field Maintenance and Minor Repair Manual
(Manual No. 170, ATA REF 61-13-70)
Hartzell Propeller Ice Protection System Manual (Manual No. 180, ATA REF 30-61-80)

Hard landing The Raisbeck/Hartzell Swept Turbofan Propellers, Five-Blade Swept Turbofan
Propellers, and Quiet Turbofan Propellers are to be inspected and maintained in
accordance with the applicable documents:
Beechcraft King Air/Super King Air Maintenance Manual
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 147, ATA REF 61-00-47)
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 149, ATA REF 61-00-49)
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 486, ATA REF 61-00-86)
Hartzell Composite Propeller Blade Field Maintenance and Minor Repair Manual
(Manual No. 170, ATA REF 61-13-70)
Hartzell Propeller Ice Protection System Manual (Manual No. 180, ATA REF 30-61-80)

Encountering The Raisbeck/Hartzell Swept Turbofan Propellers, Five-Blade Swept Turbofan

turbulent air Propellers, and Quiet Turbofan Propellers are to be inspected and maintained in
accordance with the applicable documents:
Beechcraft King Air/Super King Air Maintenance Manual
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 147, ATA REF 61-00-47)
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 149, ATA REF 61-00-49)
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 486, ATA REF 61-00-86)
Hartzell Composite Propeller Blade Field Maintenance and Minor Repair Manual
(Manual No. 170, ATA REF 61-13-70)
Hartzell Propeller Ice Protection System Manual (Manual No. 180, ATA REF 30-61-80)

Inspection after The Raisbeck/Hartzell Swept Turbofan Propellers, Five-Blade Swept Turbofan
lightning strike Propellers, and Quiet Turbofan Propellers are to be inspected and maintained in
accordance with the applicable documents:
Beechcraft King Air/Super King Air Maintenance Manual
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 147, ATA REF 61-00-47)
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 149, ATA REF 61-00-49)
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 486, ATA REF 61-00-86)
Hartzell Composite Propeller Blade Field Maintenance and Minor Repair Manual
(Manual No. 170, ATA REF 61-13-70)
Hartzell Propeller Ice Protection System Manual (Manual No. 180, ATA REF 30-61-80)

Revision AM 78
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

Propellers Special Inspections (Continued)

CONDITION INSPECTION REQUIREMENT

Inspection after The Raisbeck/Hartzell Swept Turbofan Propellers, Five-Blade Swept Turbofan
sudden Propellers, and Quiet Turbofan Propellers are to be inspected and maintained in
stoppage accordance with the applicable documents:
Beechcraft King Air/Super King Air Maintenance Manual
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 147, ATA REF 61-00-47)
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 149, ATA REF 61-00-49)
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 486, ATA REF 61-00-86)
Hartzell Composite Propeller Blade Field Maintenance and Minor Repair Manual
(Manual No. 170, ATA REF 61-13-70)
Hartzell Propeller Ice Protection System Manual (Manual No. 180, ATA REF 30-61-80)

Inspection after The Raisbeck/Hartzell Swept Turbofan Propellers, Five-Blade Swept Turbofan
deploying Propellers, and Quiet Turbofan Propellers are to be inspected and maintained in
landing gear accordance with the applicable documents:
above critical Beechcraft King Air/Super King Air Maintenance Manual
speed Hartzell Propeller Owner’s Manual and Logbook (Manual No. 147, ATA REF 61-00-47)
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 149, ATA REF 61-00-49)
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 486, ATA REF 61-00-86)
Hartzell Composite Propeller Blade Field Maintenance and Minor Repair Manual
(Manual No. 170, ATA REF 61-13-70)
Hartzell Propeller Ice Protection System Manual (Manual No. 180, ATA REF 30-61-80)

Operation in or The Raisbeck/Hartzell Swept Turbofan Propellers, Five-Blade Swept Turbofan

around Propellers, and Quiet Turbofan Propellers are to be inspected and maintained in
volcanic ash accordance with the applicable documents:
Beechcraft King Air/Super King Air Maintenance Manual
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 147, ATA REF 61-00-47)
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 149, ATA REF 61-00-49)
Hartzell Propeller Owner’s Manual and Logbook (Manual No. 486, ATA REF 61-00-86)
Hartzell Composite Propeller Blade Field Maintenance and Minor Repair Manual
(Manual No. 170, ATA REF 61-13-70)
Hartzell Propeller Ice Protection System Manual (Manual No. 180, ATA REF 30-61-80)

Revision AM 79
Document No. 85-120
Maintenance Manual and
Instructions for Continued Airworthiness for
Raisbeck Systems as installed on King Air and Super King Air Aircraft

05-72-00-21 Ram Air Recovery System Special Inspections

Ram Air Recovery System Special Inspections

INSPECTION
CONDITION INSPECTION REQUIREMENT
INTERVAL

Operation in Inspect components for condition and security. Perform Daily

atmospheres of high salt an external engine wash, to include the Ram Air Recovery
content System Ice Shedder Screen, in accordance with the
maintenance schedule set forth in the applicable Pratt &
Whitney Canada Maintenance Manual.

Operation in Inspect components For condition and security. Perform Daily

atmospheres of high an external engine wash, to include the Ram Air Recovery
industrial air pollution System Ice Shedder Screen, in accordance with the
maintenance schedule set forth in the applicable Pratt &
Whitney Canada Maintenance Manual.

Operation in areas of Inspect components for condition and security. Perform Daily
high dust content an external engine wash, to include the Ram Air Recovery
System Ice Shedder Screen, in accordance with the
maintenance schedule set forth in the applicable Pratt &
Whitney Canada Maintenance Manual.

Operation in areas of Inspect components for condition and security. Perform Daily
high humidity an external engine wash, to include the Ram Air Recovery
System Ice Shedder Screen, in accordance with the
maintenance schedule set forth in the applicable Pratt &
Whitney Canada Maintenance Manual.

Operation from very soft Inspect for condition and security. Daily
or unusual terrain

Hard landing Inspect for condition and security. As required

Encountering turbulent Inspect for condition and security. As required

air

Inspection after lightning Inspect area of suspected lightning strike for security and As Required
strike condition. Repair or replace damaged components as
required.

Operation in or around Inspect components for condition and security. Perform Daily
volcanic ash an external engine wash, to include the Ram Air Recovery
System Ice Shedder Screen, in accordance with the
maintenance schedule set forth in the applicable Pratt &
Whitney Canada Maintenance Manual.

Revision AM 80